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Ramesh, V (2002) Least squares grid free kinetic upwind method. ["eprint_fieldopt_thesis_type_phd" not defined] thesis, Indian Institute of Science, Bangalore.
Siva Kumar, K. and Sharanappa , Sajjan V (2011) Unsteady Compressible Flow over Heaving Bodies Using an Implicit RANS Solver. In: 2011 International Conference on Mechanical and Aerospace Engineering (CMAE 2011), March 21-23, 2011, SRM University, Modi Nagar Campus,Delhi-Meerut Road, Sikrikalan Modi Nagar, Gazhiabad, Uttar Pradesh - 201 204.
ALD, (1999) Annual R & D Report of the Aerospace Electronics and Systems Division for 1998-1999. Technical Report. National Aerospace Laboratories, Bangalore, India.
ALD, - (1992) Annual report 1991 of the aerospace electronics and systems division. Technical Report. National Aeronautical Laboratory, Bangalore, India.
ANON, - (1987) Captive trajectory system for the 1.2m trisonic wind tunnel - a broad outline and technical specification. Project Report. National Aerospace Laboratories, Bangalore.
Achar, Narahari BN (1963) Optimisation of tin can thermal ballast requirements of blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Acharya, YVG (1961) Aerodynamic design of a variable mace number supersonic nozzle for the 4quot;x4quot; trisonic tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Acharya, YVG (1961) Aerodynamic design of a variable mach number supersonic nozzle for the 4'X4' trisonic tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Acharya, YVG (1961) Note on the air dryer for the 4'X 4' trisonic tunnel. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Acharya, YVG (1961) Note on the choice of ventilating walls for the transonic test section of the 4' X 4' trisonic tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Adiga, BS and Muralidhar, SJ and Ramesh, C and Aravind, (1991) PC based A 320 quick access recorder readout facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Aerodynamics Division, - (1963) 4ftx4ft Trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Aerospace Electronics amp; Systems Division, -- (1994) Annual R amp; D Report of the Aerospace Electronics and Systems Division for 1993. Technical Report. National Aerospace Laboratories, Bangalore, India.
Ahmed, Sajeer (1987) Effectiveness of vortex plate on the aerodynamic characteristics of MiG-21M aircraft model. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer (1987) Surface pressure measurements in the strap-on boosters interference region of 1/180 scale PSLV configuration at supersonic speeds. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Mathur, NB and Manisankar, C (2011) Evaluation of aerodynamic performance of sidewall compression intake relevant to air breathing propulsion vehicles for intake flow entry at M = 3.5. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Selvarajan, S (1987) Steady pressure measurements in the strap on boosters interference region of 1/40 scale PSLV configuration. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Selvarajan, S (1986) Unsteady Pressure Measurements on Scaled Configurations of ASLV. Project Report. NAL, Bangalore.
Ahmed, Sajeer and Selvarajan, S and Varambally, BS and Sivaramakrishnan, AE and Pandyan, S (1987) Steady pressure measurements in the strap-on booster interference Region of 1/20 scale aslv configuration. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Sudhakar, (2007) Flows on delta wing. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Sudhakar, S (2009) Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations. Project Report. National Aerospace Laboratories, Bangalore.
Anand, kumar (1988) Euler solutions with a multi-block structured code 13; 13;. Journal of Aeronautical Society of India, 40. pp. 89-95.
Anju, Sharma (2021) Development of LabVIEW based mass flow plug control for wind tunnel application. In: AIP Conference Proceedings 2316.
Anon, - (1986) Captive Trajectory System - A Preliminary Report to the Technical Evaluation Com. Project Report. NAL, Bangalore.
Anon, - (1986) General specifications for a diesel engine compressor system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Anon, - (1987) Missile Aerodynamics Design Manual. Project Report. NAL, Bangalore.
Aravind, M and Kumar, CVS and Pai, BR and Kumar, HSR (2015) Experimental study of pitch damping in a coaxial model helicopter. In: ARF 2015 - 4th Asian-Australian Rotorcraft Forum, 15-18 November 2015, Bangalore, India.
Archana, Hebbar P (2010) Literature survey on Human Factor Engineering Aspects in aviation. Project Report. National Aerospace Laboratories, Bangalore.
Archana, Hebbar P (2010) Literature survey on Human Factor Engineering Aspects in aviation. Project Report. National Aerospace Laboratories, Bangalore.
Archana, Hebbar P and Metilda, J and Srikanth, K P (2009) Design and development of real time plotting software (RTPLOT). Technical Report. NAL.
Arivoli, D and Dodamani, Ravi and Ramesh, G and Ahmed, Sajeer (2009) Preliminary wind tunnel studies on Micro-Air Vehicles. Project Report. National Aerospace Laboratories, Bangalore.
Arivoli, D and Singh, Ishan (2015) Self-Activated Movable Flaps on Low Aspect Ratio Wings at Low Reynolds Numbers. In: International Micro Air Vehicle Conference and Flight Competition, Sept. 2015, Aachen, Germany.
Arivoli, D and Singh, Ishan and Suriyanarayanan, P (2020) Rudimentary emulation of covert feathers on low-ar wings for poststall lift enhancement. AIAA Journal, 58 (2). pp. 501-516. ISSN 00011452
Arokkiaswamy, A and Kanagarajan, V (1985) Estimation of error in measurement of force and moment coefficients of wind tunnel models. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Arora, NL (1964) Calibration of the 5 in. x 5 in. induction tunnel with 2 in. x 10 in. test section having normal hole perforated walls and without plenum auxiliary suction. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Arun Kumar, P and Verma, SB and Rathakrishnan, E (2015) An experimental study of subsonic and sonic jets controlled by air-tabs. In: 51st AIAA/SAE/ASEE Joint Propulsion Conference.
Ashoka, BS and Seenappa, - and Chandran, AP and Kanakamuthu, (2011) System Architecture of a 2 kW Variable speed generator test bed. Technical Report. National Aerospace Laboratories, Bangalore, India.
Ashwin, S and Karthikeyan, N (2013) Prediction of Launch Vehicle Noise during Lift-off using Modified Eldred’s Method. In: The 14th Asian Congress of Fluid Mechanics, 15-19 Oct 2013, Hanoi and Halong, Vietnam.
Ashwin Kumar, S and Karthikeyan, N and Venkatakrishnan, L (2015) Effect of inverted triangular tabs on mitigation of jet noise from axisymmetric convergent nozzles. In: 21st AIAA/CEAS Aeroacoustics Conference, AIAA AVIATION Forum, 22-26 June 2015, Dallas, TX.
Babu, Mallesh and Lokesha, H and Veena, S and Rathod, JA (2015) Controlling the micro air vehicle through voice instructions. International Journal of Computer Engineering and Technology (IJCET), 6 (4). pp. 21-27. ISSN 0976-6375
Balakrishna, S (1970) Wind tunnel pressure regulating systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Balakrishna, S and Niranjana, T (1987) Wind tunnel dynamic flying study of the pitching moment derivatives of the Standard Dynamics Model in active control. In: AIAA Atmospheric Flight Mechanics Conference, 17-19 Aug 1987, United States.
Balakrishna, S and Niranjana, T and Rajan, SR (1986) A low speed tunnel semi-free dynamic flying study of the high angle of attack pitch derivatives of HF-24 using MILE procedure. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Balakrishna, S and Niranjana, T and Rajan, SR and Rajamurthy, MS (1991) Dynamic flying investigations on 1/13.5 NALLA Model (Longitudinal Results). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Balakrishna, S and Srinathkumar, S (1963) Pressure transducers using the linear differential transformer. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Balaraju, JN and Jahan, SM and Anadan, C and Rajam, KS (2006) Studies on electroless Ni-W-P and Ni-W-Cu-P alloy coatings using chloride-based bath13;. Surface amp; Coatings Technology, 200 (16-17). pp. 4885-4890.
Balaraju, JN and Kalavati, - and Rajam, KS (2006) Influence of particle size on the microstructure, hardness and corrosion resistance of electroless Ni-P-Al2O3 composite coatings13;. Surface and Coatings Technology, 200 (12-13). pp. 3933-3941.
Balasingh, C and Gururaja, B and Rohini, S (1993) Residual stress distribution in the As-received aluminum-lithium alloy sheet. Technical Report. National Aerospace Laboratories, Bangalore, India.
Balasingh, C and Singh, AK (1969) Measurement of stress: Photographic method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Balasubramanian, TS (1982) Flag-lag stability of helicopter rotor blads in hover and forward flight. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Barshilia, Harish C and Rajam, KS (2002) Characterization of Cu/Ni multilayer coatings by nanoindentation and atomic force microscopy. Surface and Coatings Technology, 155. pp. 195-202.
Barshilia, Harish C and Rajam, KS (2004) Nanoindentation and atomic force microscopy measurements on reactively sputtered TiN coatings. Bulletin of Materials Science, Vol. 2 (No. 1). pp. 35-41.
Barshilia, Harish C and Rajam, KS (2004) Raman spectroscopy studies on the thermal stability of TiN, CrN, TiAlN coatings and nanolayered TiN/CrN, TiAlN/CrN multilayer coatings. Journal of Materials Research, 19 (11). pp. 3196-3205.
Barshilia, Harish C and Surya Prakash, M and Aithu, Poojari and Rajam, KS (2004) Corrosion Behaviour of TiN/a-C Superhard Nanocomposite Coatings Prepared by a Reactive DC Magnetron Sputtering Process. Transactions of the Institute of Metal Finishing, 82 (4). pp. 1-7.
Barshilia, Harish C and Surya Prakash, M and Sridhara Rao, DV and Rajam, KS (2004) Superhard nanocomposite coatings of TiN/a-C prepared by reactive DC magnetron sputtering. Surface amp; Coatings Technology, 195 (2-3). pp. 147-153.
Basappa, - and Jategaonkar, RV (1995) Aspects of Feed Forward Neural Network Modeling and its Application to Lateral-Directional Flight Data. Technical Report. National Aerospace Laboratories, Bangalore, India.
Baskaran, AR and Srikantan, KV (1986) Electronic private automatic branch exchange facilities for Wind Tunnel Centre Campus of NAL. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Basu, AJ and Narasimha, R and Prabhu, A (1993) Vortex simulation of turbulent mixing layers13;. Sadhana, 18. pp. 943-962. ISSN 0256-2499
Basu, AJ and Sinha, UN and Narasimha, R (1993) Vorticity in transitional axisymmetric wakes by direct numerical simulation. In: Proceedings of the Internationl Symposium on Recent Advances in Aerospace Sciences and Engineering, 2-15 Dec 1992, Bangalore, India.
Bera, Rajendra K (1989) An Accurate method for calculating the initial development of vortex sheets. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1976) Aircraft external stores wind tunnel techniques and scaling laws. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1975) Functional approximations to experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1975) Functional approxmations to experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1989) New look at Theodorsen's method in aerofoil theory. International Journal for Numerical Methods in Fluids, 9 (3). pp. 251-262. ISSN 0271-2091
Bera, Rajendra K (1976) On simulation and evaluation of aircraft handling qualities. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1988) On the self-induced motion of vortex sheets. International Journal for Numerical Methods in Fluids, 8. pp. 759-768. ISSN 0271-2091
Bera, Rajendra K (1977) Remarks on thin airfoil theory. Journal of Aircraft, 14 (5). pp. 508-509. ISSN 0021-8669
Bera, Rajendra K (1974) Slender delta wing with conical camber. Journal of Aircraft, 11. pp. 245-247. ISSN 0021-8669
Bera, Rajendra K (1974) Some remarks on the solution of the lifting line equation. Journal of Aircraft, 11 (10). pp. 647-648. ISSN 0021-8669
Bera, Rajendra K (1974) Warping of delta wings for minimum drag. Journal of Aircraft, 11 (12). pp. 777-779. ISSN 0021-8669
Bera, Rajendra K and Ramachandra, SM (1979) Conically cambered delta wings in supersonic flow. I - Basic solutions. Journal of Aeronautical Society of India, 29 (3, 4). pp. 87-94.
Bera, Rajendra K and Ramachandra, SM (1979) Conically cambered delta wings in supersonic flow. II - Optimal solutions. Aeronautical Society of India, Journal, 29. pp. 145-148.
Bera, Rajendra K and Ramachandra, SM (1974) Method of orthogonal loadings - A fresh look. Journal of Aircraft, 11 (10). pp. 650-651.
Bhagawan, BS and Parameswaran, V and Rajeswari, Ramamurthy S and Seshadri, SN and Sridhar, JK and Srinatha Sastry, CV and Yegna Narayan, K (1985) Longitudinal stability and control characteristics of MIG-21 aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Bhaumik, SK and Saikrishna, CN and Ramaiah, KV (2006) Effects of thermo-mechanical cycling on the strain response of Ni-Ti-Cu shape memory alloy wire actuator13;. Materials Science amp; Engineering A (Structural Materials: Properties, Microstructure and Processing, 428 (1-2). pp. 217-224.
Bhaumik, SK and Singh, AK (1993) Polycrystalline cubic boron nitride (PCBN) cutting tools. Technical Report. National Aerospace Laboratories, Bangalore, India.
Bhoi, SR and Suryanarayana, GK (2008) Prediction of pressure characteristics in setting chamber of 0.6m wind tunnel for supersonic testing. Technical Report. National Aerospace Laboratories, Bangalore, India.
Bikshapathi, Manupati and Karthik, N and Buddhadeb, Nath and Gopinath, PR and Mohan, SR and Koner, D (2009) Study of flow unsteadiness in a bifurcated Y-Shaped duct for a typical combat aircraft model. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, Bangalore,India.
Brahma, KK (2001) Seismic qualification of directional valve. Project Report. National Aerospace Laboratories, Bangalore.
Chakrabartty, SK (2005) Role Of Computational Fluid Dynamics In The Design Of Aerospace Configurations. Journal of Aerospace Sciences amp; Technology, 57 (1). pp. 24-32. ISSN 0971-950X
Chakrabartty, SK and Desai, SS and Prabhu, DK and Saxena, SK and Majumdar, Sekhar (1993) Fluid Dynamics Symposium in honour of Professor R.Narasimha on his 60th birthday. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 Jul 1993, Bangalore, India.
Chakrabartty, SK and Dhanalakshmi, K (1995) Computation of transonic flows with shock-induced separation using algebraic turbulence models. AIAA Journal, 33 (10). pp. 1979-1981.
Chakrabartty, SK and Dhanalakshmi, K (1993) A vertex-based finite-volume algorithm for the Navier-Stokes equations. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.
Chakrabartty, SK and Subramanian, NR (1980) Low-frequency and small perturbation equation for transonic flow past wings. AIAA Journal, 18. pp. 1147-1149. ISSN 0001-1452
Chandra, R and Basava Raju, B (1975) Large deflection vibration of angle ply laminated plates. Journal of Sound and Vibration, 40. pp. 393-408. ISSN 0022-460X
Chandra, R and Kumar, M (1978) Joint allowables of some composite-composite joints. In: Proceedings of the Symposium on Jointing in Fibre Reinforced Plastics, 4-5 Sep 1978, England, UK.
Chandra, Ramesh and Guruprasad, K and Dwarakanath, K (1988) Energy release rates in patched cracked plates. Engineering Fracture Mechanics, 31 (5). pp. 719-732. ISSN 0013-7944
Chandran, AP and Kanakamuthu, and De, Manabendra M and Ashoka, BS and Dayananda, GN (2011) Procedure for commissioning and operation of the NMITLI 500kW Wind turbine system. Technical Report. National Aerospace Laboratories, Bangalore, India.
Channa Raju, - (1998) Free Piston Shock Tunnels: A Survey. Technical Report. National Aerospace Laboratories, Bangalore,India.
Channa Raju, - and Viswanath, PR (2003) Pressure Sensitive Paint measurements in NAL 1.2m blowdown wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Chetty, Shyam and Marchand, M (1993) Frequency domain identification of lower order equivalent systems. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.
Chetty, Shyam (2015) National Aerospace Laboratories, Bengaluru. Current Science, 108 (5). pp. 792-796. ISSN 00113891
Chidambaranathan, M and Verma, SB and Rathakrishnan, E (2019) Control of incident shock-induced boundary-layer separation using steady micro-jet actuators at M∞ = 3.5. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 233 (4). pp. 1284-1306. ISSN 09544100
Chopra, I (1975) Flutter of a panel supported on an elastic foundation. AIAA Journal, 13 (5). pp. 687-688. ISSN 0001-1452
Chopra, I (1974) Vibration of stepped thickness plates. International Journal of Mechanical Sciences, 16. pp. 337-344. ISSN 0020-7403
Chopra, I and Durvasula, S (1972) Vibration of simply-supported trapezoidal plates: I - Symmetric Trapezoids. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Chopra, I and Durvasula, S (1972) Vibration of simply-supported trapezoidal plates: II - Unsymmetric Trapezoids. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Chutkey, K and Suriyanarayanan, P. and Venkatakrishnan, L. Near wake field of circular cylinder with a forward splitter plate. Journal of Wind Engineering and Industrial Aerodynamics}, 173. pp. 28-38. ISSN 01676105
Chutkey, Kiran and Suriyanarayanan, P and Venkatakrishnan, L (2021) Effect of Forward Splitter Plate Leading Edge Shape on the Cylinder Flow. In: Proceedings of 16th Asian Congress of Fluid Mechanics, Singapore.
Coomar, Nilanjan and Rajani, BN and Majumdar, Sekhar (2000) Numerical computation of vortex shedding around a circular cylinder. Project Report. National Aerospace Laboratories, Bangalore, India.
Damania, RB (1986) concept study for a 80% scaled Derivative LCA. Project Report. National Aerospace Laboratories, Bangalore.
Danish, TH and Sathiyamoorthy, K and Srinivas, J and Manjunath, P (2013) Drag characterization of Strut-mounted 'Through Cavity' for scramjet applications. In: 23rd National Conference on I.C. Engine and Combustion (NCICEC 2013), 13-16 Dec. 2013, SVNIT, Surat, India.
De, Manabendra M and Ashoka, BS and Seenappa, - and Chandra, AP and Kanakamuthu, (2011) Preliminary studies of the Aero-generator for battery charging application. Technical Report. National Aerospace Laboratories, Bangalore, India.
De, Manabendra M and Kanakamuthu, and Isaac, JJ (2011) Aerodynamic design & analysis of the Innovative Tip Brake of the NMITLI 500 kW Horizontal-Axis Wind Turbine. Technical Report. National Aerospace Laboratories, Bangalore, India.
De, MM and Mathur, JS and Vengadesan, S (2021) Entropy and fractal perspectives of a flapping wing subjected to gust. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 235 (15). pp. 2165-2181. ISSN 0954-4100
De, MM and Mathur, JS and Vengadesan, S (2019) Simulation of flapping wings subjected to gusty inflow. Aeronautical Journal, 123 (1266). pp. 1170-1192. ISSN 00019240
Desai, SS (1977) Axisymetric supersonic nozzle design foelsch method. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Desai, SS (1985) Computational aerodynamics - A project proposal. Project Report. National Aerospace Laboratories, Bangalore.
Desai, SS (1971) Method of characteristics for two-dimensional and for axisymmetric flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS (1977) Notes on the concept of principal value of an integral and the finite part of an infinite integral13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS (1985) Report on a three week stay at MBB Ottobrunn. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS (1994) Viscous flow past aerofoils axisymmetric bodies and wings 13; 13;. In: CFD: Advances and Applications, 1994, India.
Desai, SS and Narayana, CL and Rangarajan, R (1985) Extension to the Panel Code NALSOP0509 to Include Design of Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment. Project Report. National Aerospace Laboratories, Bangalore.
Desai, SS and Ragarajan, R and Singh, JP and Ravichandran, KS (1988) Full-potential calculations using Cartesian grids. Aeronautical Society of India, Journal, Vol. 4. pp. 97-103.
Desai, SS and Rangarajan, R (1993) Development of full-potential codes in the decade 1983-1993. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 1993, Sikkim.
Desai, SS and Rangarajan, R (1988) Mathematical modelling and computer simulation using cartesian grid. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Rangarajan, R (1986) Prediction of viscous effects on an aerofoil using transpiration model for the effects of boundary layer and wake. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Rangarajan, R (1986) Viscous transonic flow over aerofoils using transonic full potential equation in a system of cartesian coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Rangarajan, R and Ravichandran, KS (1985) A preliminary note on the development of a three-dimensional potential code in cartesian coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Sharma, Ramachandra and Venkateshwarlu, K and Krishnamurthy, K (1982) Wall interference studies on NACA 0012 Aerofoil in the NAL 0.3m wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Viswanathan, S (1980) Design of Axisymmatrec supersonic/hypersonic nozzles. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Viswanathan, S (1980) Design of axisymmetric supersonic/hypersonic nozzles. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desai, SS and Viswanathan, S and Ramaswamy, MA (1977) Numerical evaluation of transonic wave drag. Journal of Aircraft, 14 (2). pp. 215-217. ISSN 0021-8669
Deshpande, MD (2000) Decay of Three-Dimensional Vortex Motion in an Enclosure. Project Report. National Aerospace Laboratories, Bangalore, India.
Deshpande, MD (1993) Flow Regimes in a Three-Dimensional Driven Cavity13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Deshpande, MD (2004) Improving the Accuracy of the Numerical13; Solutions by Richardson Extrapolation13;. Technical Report. National Aerospace Laboratories, Bangalore, India.
Deshpande, MD and Shankar, PN (1990) Direct Simulation of Turbulent Channel Flow. Project Report. NAL, Bangalore.
Deshpande, MD and Shankar, PN (1994) Direct numerical simulation of a complex turbulent flow. Current Science, 66 (10). pp. 767-770.
Deshpande, MD and Srinidhi, BG (2006) Mixed convection in a lid-driven cavity: appearance of bifurcation, periodicity and hysteresis13;. Current Science, 89 (10). pp. 1720-1728.
Deshpande, MD and Srinidhi, BG (2004) Mixed convection in a lid-driven three-dimensional cavity. Technical Report. National Aerospace Laboratories, Bangalore, India.
Deshpande, P and Vishwasrao, A (2021) Kinematics and dynamics of pitching flexible panels in a quiescent fluid. Journal of Fluid Mechanics, 922. ISSN 00221120
Deshpande, P J and Modani, A (2019) Experimental investigation of fluid–structure interaction in a bird-like flapping wing. Journal of Fluids and Structures, 91. ISSN 08899746
Desikan, KS (1989) Design and commissioning of 0.6M transonic tunnel - mechanical system (project closing report). Project Report. National Aerospace Laboratories, Bangalore.
Desikan, KS (1974) Design of acoustic mufflers for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desikan, KS (1976) Design of prototype intake silencer for 60mw fd fan (BHEL). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desikan, KS (1972) Slope and deflection of 4-FT.Tunnel model support stings. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Desikan, KS and Mohan, KH (1990) Fabrication of 1 /20th scale high speed wind tunnel model of MiG-27 (project closure report). Project Report. National Aerospace Laboratories, Bangalore.
Dhanalakshmi, K and Mathur, JS and Singh, Manish K (2010) Aerodynamic Load Computation for MiG-29 Aircraft. Project Report. NAL, Bangalore.
Divakar, C and Mohan, Murali (1984) The kinetics of pressure induoed fcc-bcc transformation in ytterbium. Journal of Applied Physics., 56. pp. 2337-2340.
Divya , S and Singh, DB and Lakshmikanthiah, Y and Rao, K Prasad (2011) Development of 8-Channel wireless data acquisition system for wind tunnel application. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Dongare, V and Majeed, M (2015) Lateral-directional aerodynamics parameter estimation using neural partial differentiation. In: Cognitive Computing and Information Processing (CCIP), 2015 International Conference on, 3-4 March 2015, Noida, India.
Durai, Arivoli (2014) Experimental Investigation of Lift and Drag Characteristics of a Typical MAV under Propeller Induced Flow. International Journal of Micro Air Vehicles, 6 (1). ISSN 1756-8293
Durai, Thulasi D and Viswamurthy , SR and Chaplod, Saniya and Dhami, Govind Singh and Smiti, Maini and Abhimanyu, Sharma and Krishnamoorthy, K (2011) Development of a blended wing configuration MAV. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Dutt, HNV (1989) Analysis of multi-element airfoils by a vortex panel method. AIAA Journal, 27 (5). pp. 658-660. ISSN 0001-1452
Dutt, HNV (1987) Analysis of two-dimensional multi-component airfoils in viscous flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Dutt, HNV (1988) Comment on 'Computation of the potential flow over airfoils with cusped or thin trailing edges'. AIAA Journal, 26 (1). pp. 122-123. ISSN 0001-1452
Dutt, HNV (1986) Fortran program for calculating the static longitudinal aerodynamic characteristics of wing-body-tail configurations including vortex lift from sharp edges. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Dutt, HNV (1985) Parametric bi-cubic surface patch for computer aided geometric design of aircraft and/or other three-dimensional geometries. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Dutt, HNV and Jacob, K (1989) Viscous subsonic flow computation for wings with flaps for high-lift. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Dutt, HNV and Jacob, K (1993) Viscous subsonic flow computation for wings with flaps for high-lift. Journal of Aircraft, 30 (1). pp. 141-143. ISSN 0021-8669
Dutta, PK and Dutta, Vimala and Sharanappa, Sajjan V (2007) Rans computation of flow past wind turbine blades. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Dutta, Vimala (1985) Computational requirements for the solution of navier-stokes equations. Project Report. National Aeronautical Laboratory, Bangalore, India.
Dutta, Vimala and Ramamoorthy, P (1988) Validation of a NASA code for determining the viscous supersonic flow past a pointed body of revolution. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Dwarakanath, GS and Ramamoorthy, P and Rao, DM (1974) Evaluation of the transonic wave drag integral with particular reference to a real aircraft. Technical Report. National Aeronautical Laboratory, Bangalore,India.
FMCD, - (1991) Annual R amp; D report of FMCD for 1990. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Farook, MA and Ramanaiah, B and Gopalan, R (1990) Static testing of DO-228 Composite rudder - a preliminary report. Project Report. National Aerospace Laboratories, Bangalore.
Ganguli, Ranjan and Thakkar, D and Viswamurthy, SR (2016) Dynamic stall alleviation using active twist. Advances in Industrial Control. pp. 221-249. ISSN 14309491
Ganguli, Ranjan and Thakkar, D and Viswamurthy, SR (2016) Flap configuration and control law. Advances in Industrial Control. pp. 81-101. ISSN 14309491
Gireesh, Yanamashetti and Singh, DB and Suryanarayana, GK and Mukherjee, Rinku (2021) Effect of aerospike on unsteady transonic flow over a blunt body. Journal of Spacecraft and Rockets, 58 (6). pp. 1806-1818. ISSN 00224650
Gireesh, Yanamashetti and Suryanarayana, GK and Mukherjee, Rinku (2017) Development of Flow over Blunt-Nosed Slender Bodies at Transonic Mach Numbers. Journal of Physics: Conference Series, 822 (1). 012071. ISSN 1742-6596
Giridhar, Babu Y and Felix, J and Krishnamoorthy, V (2009) Experimental investigation of effusion cooling performance on flat plates. Technical Report. NAL.
Giridhar, Babu Y and Gururaj, L and Ashok Babu, TP and Felix, J and Sreenivas Rao, VK and Vinodkumar, N (2013) Experimental and Numerical Investigation of Effect of Blowing Ratio on Film Cooling Effectiveness and Heat Transfer Coefficient over a Gas Turbine Blade Leading Edge Film Cooling Configurations. In: ASME 2013 GAS TURBINE INDIA CONFERENCE, 5-6 Dec 2013, CSIR-NAL, Bangalore.
Girigoswami, H and Mohan, K (1986) Novel loading device for testing high power drive systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Girija, G and Basappa, - and Raol, JR and Padma, Madhuranath (2001) Estimation methods for determination of drag characteristics of fly-by-wire aircraft. Defence Science Journal, 51 (1). pp. 83-92.
Girija, G and Kamali, C (2005) Real Time Aerodynamic Parameter Estimation Schemes- a Survey, Implementation and Comparison. Project Report. National Aerospace Laboratories.
Girija, G and Raol, JR (1993) Parameter estimation for unstable and augmented systems using recursive mixed estimation method. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.
Godbole, AK and Sinha, UN (1986) Pressure distribution and wave drag for a body of revolution using conservative and non-conservative schemes. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopalakrishnan, AR and Ramamoorthy, P (1977) Determination of pressure distribution on a finite wing by kuchemann and weber method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopalakrishnan, V (1994) Capacitance meters and transistor tester. Modelling, Measurement amp;amp; Control, 53 (3). pp. 37-39.
Gopalratnam, Girija and Raol, JR and Jategaonkar, RV (1993) Aerodynamic parameter estimation from dynamic maneuvers by two step methodology. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopinath, N and Narayan, KY (1988) Wind tunnel tests on LCA stage 4 configuration. Project Report. National Aerospace Laboratories, Bangalore.
Gopinath, R (1966) On Maslen's solution for inviscid flow past blunt bodies. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopinath, R (1983) Tunnel interference from pressure measurements on control surfaces. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopinath, R and Shantha Kumari, S (1987) An Assessment of 2-D Wall Interference from Pressure Measurements on the Airfoil and on the Control Surface. Project Report. National Aerospace Laboratories, Bangalore.
Gopinath, R and Shantha Kumari, S and Sridharan, R (1987) Tests on 3 NACA 0012 airfoil models of DFVLR in the NAL 0.3m tunnel: An assessment of 2-D wall interference. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopinath, R and Subramanian, NR (1968) Asymptotic theory of the blunted wedge at hypersonic speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gopinath, R and Viswanathan, S and Desai, SS (1991) Preliminary Results on the Influence of Tunnel Wall Boundary Conditions on 2-D Transonic Full Potential Code. Technical Report. National Aerospace Laboratories, Bangalore, India.
Gupta, Ramesh P (1974) New design of pressure probe as a skin friction gauge. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Gupta, Ramesh P (1973) Non-nulling calibration of asymmetric probe and its application to measurements in cascade wakes. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Guruganesh, R and Bandyopadhyay, B and Arya, H and Singh, GK (2016) Design of autopilot control laws for MAV using super twisting control. IFAC-PapersOnLine, 49 (1). pp. 730-735. ISSN 24058963
Haque, CI and Mahalingam, S (1971) A computer programe for the analysis of the subsonic cascade tunnel data. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Hebbar, KS (1981) Experimental study of incompressible mean and turbulence flow fields on and behind a symmetric aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Hebbar, KS and Melnik, WL (1978) Wall region of a relaxing three-dimensional incompressible turbulent boundary layer. Journal of Fluid Mechanics, 85. pp. 33-56. ISSN 0022-1120
Hebbar, KS and Ramakrishnan, SV and Yajnik, KS (1982) Experimental study of flow past a surface mounted cylinder having a hemisperical end. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Hebbar, Sheshagiri K and Paranjpe, PA (1969) Skin friction and laminar-sublayer thickness compressible turbulent boundary layers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Hebbar, Sheshagiri K and Sridhara, K and Paranjpe, PA (1970) Performance of conical jet nozzles in terms of discharge coefficient. Journal of Aeronautical Society of India, 22 (1). pp. 3-9.
Hemant , Sharma (2010) Feasibility Study Conducted for the Development of an Autonomous mini Unmanned Air Vehicle. Project Report. National Aerospace Laboratories, Bangalore.
Hemant , Sharma and Suraj, CS and Roshan, Antony and Ramesh, G and Sajeer, Ahmed and Prasobh, Narayan Design of a High Altitude Fixed Wing Mini UAV – Aerodynamic Challenges. In: ICIUS 2013, 25 Sep 2013, Jaipur.
Hossain, J and Tran, LV and Carpenter, C and Wang, W and Verma, SB and Kapat, JS (2013) Numerical study of enhancement of regenerative cooling using ribs - AIAA 2013-3996. In: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 14-17 Jul 2013, San Jose, CA, USA.
Hussain, GF and Nasser, AS and Nawaz, MM and Mondal, BK and Karthikeyan, N (2013) Effect of perforated tabs on the noise field of an axisymmetric jet. Applied Mechanics and Materials, 307. pp. 250-256. ISSN ISSN: 1662-7482
ISS Section, - (1996) Material for CSlR Annual Report 1995-96. Technical Report. National Aerospace Laboratories, Bangalore, India.
Ibrahim, K (2003) Selecting fuel fraction, propeller diameter and fuselage length for military propeller trainers 13;. In: 21st AIAA Applied Aerodynamics Conference, 23-26 Jun 2003, Orlando, FL.
Irani, PA and Iya, Sridhar K (1963) Aerodynamic noise in aircraft and wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Isaac, JJ (1976) Prediction of the effective blockage of flame stabilizers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Isaac, JJ (1976) Stability criteria of jet flame holders. In: 3rd National Conference on Internal Combustion Engines and Combustion, 10-12 Dec 1976, Roorke, India.
Isaac, JJ and Paranjpe, PA (1978) Cycle optimization a solar turbopack. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Isaac, JJ and Paranjpe, PA (1978) Cycle optimization for a solar turbopack (turbine water pump utilizing Rankine cycle). In: Proceedings of the International Solar Energy Congress on Sun: Mankind's future source of energy, 16-21 Jan 1978, New Delhi, India.
Ismail, Shaik and Pashilkar, AA and Ramakalyan, Ayyagari and Narasimhan, Sundararajan (2014) Improved neural-aided sliding mode controller for autolanding under actuator failures and severe winds. Aerospace Science and Technology, 33. pp. 55-64. ISSN 1270-9638
Ismail, Shaik and Singh, Jatinder (2005) Global Nonlinear Aerodynamic Model Validationby 6 DOf Simulation- Application to F-16. Technical Report. National Aerospace Laboratories,Bangalore, Bangalore, India.
Iyer, RV and Vijayan, Kalyani (1993) X-ray analysis of the thermal decomposition behaviour of Kevlar fibres. Technical Report. National Aerospace Laboratories, Bangalore, India.
Jain, Ashok K (1982) Performance Evaluation of Two-dimensional External Compression Inlet Configuration at Supersonic Speeds13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Jain, Nikhil (2005) EM Design and Applications of Metamaterials. Technical Report. National Aerospace Laboratories, Bangalore.
Jaman, PM and Singh, AK (1992) Pressure testing of drop tank components. Project Report. National Aerospace Laboratories, Bangalore.
Janardhan, S and Rajagopal, KS and Muralidharan, SK (1975) Curve fitting with end-constraints based on a modification of Hiroshi-Akima's method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Janardhana Rao, N and Adolf, Zach (1993) Developments on the HP Statistical Library Analysis Software. Technical Report. National Aerospace Laboratories, Bangalore, India.
Jategaonkar, RV and Balakrishna, S (1986) Effects of flap position on longitudinal parameters of HFB-320. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Jategaonkar, RV and Viswanathan, R and Rao, Vasudeva NA (1980) A self excitation and control system for wind tunnel dynamic stability measurements. Journal of Aeronautical Society of India, 32. pp. 37-44.
Jayaprakash, C and Sathiyamoorthy, K and Khan, AA and Venu, G and Venkat Iyengar, S and Srinivas, J and Prateesh Kumar, P and Manjunath, P (2013) Development of Mach 3.6 water cooled facility nozzle. In: National Propulsion Conference, Feb 2013 , Chennai.
Jayaraman, V (1987) Wind .-Turinel Testing . on underwater Axisymmetric body at Angle of Attack,-Part II Experimental investigation on an Axisymmetric body with ogive nose. Project Report. National Aerospace Laboratories, Bangalore.
Jayaraman, V (1987) Wind Tunnel Testing on Underwater Axisymmetric Bodies at Angle of Attack - Part IV - Surface Pressure Measurements on the Model at Negative Incidences. Project Report. National Aerospace Laboratories, Bangalore.
Jayaraman, V (1987) Wind tunnel testing on underwater axisymmetric bodies at angle of attack Part III - Experimental investigation on an axisymmetric Body with Blunt Nose. Project Report. National Aerospace Laboratories, Bangalore.
Jayaraman, V and Dutt, HNV (1993) Low speed experimental study on a high-lift system Used for LTA. Project Report. National Aerospace Laboratories, Bangalore.
Jayasingh, EM and Tantria, TA and Bhaskaran, TA and Biswas, SK and Ramasesha, Sheela K (2002) Performance of monolithic and TiBlt;subgt;2lt;/subgt; reinforced MoSilt;subgt;2lt;/subgt; in dry sliding contact with steel. Materials Letters, 53 (4-5). pp. 379-383.
Joshi, P. and Rajaei, H. and Kunnen, R.P. and Clercx, H.J.H. (2017) Heat transfer in rotating Rayleigh-Bénard convection with rough plates. Journal of Fluid Mechanics, 830. ISSN 00221120
Jyothi Kumar, Puttam (2013) Implementation and Testing of Overset Grid Capability for Supersonic Flows. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2013), 21 Nov 2013, Hyderabad, India.
Kailash, K and Prakash, S (1992) PC implementable finite element programme for design and optimisation of Lattice towers of wind machines. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kailash, K and Prakash, S (1989) Structural analysis of an isolated SAMIRA blade. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kaliraj, KR and Yepuri, GB and Sarasamma, JJ and Kumar, K and Jesuraj, F (2019) Parametric studies on gas turbine labyrinth seal for the secondary air flow optimization at static and rotating conditions. In: ASME 2019 Gas Turbine India Conference, GTINDIA 2019, December 5–6, 2019, Chennai, Tamil Nadu, India.
Kalyana Raman, V (1961) Report on the cooling water plant at hindustan antibiotics Ltd. Pimpri. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kamali, C and Girija, G (2005) Real Time Aerodynamic Parameter Estimation Schemes- A Survey, Implementation and Comparison. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kamali, C and Pashilkar, AA (2009) Nonlinear aerodynamic model structure determination using statistical measures. Project Report. National Aerospace Laboratories, Bangalore.
Kamali, C and Pashilkar, AA (2006) Real Time Parameter Estimation For Reconfigurable Control Of Unstable Aircraft. Project Report. National Aerospace Laboratories.
Kamali, C and Pashilkar, AA (2006) Study of RLS for Stability Margin Evaluation and Post Failure Data Analysis. Project Report. National Aerospace Laboratories, Bangalore.
Kamali, C and Jain, S and Saraf, Amitabh (2016) Novel method for static pressure calibration using Unscented Kalman Filter. IFAC-PapersOnLine, 49 (1). pp. 646-651. ISSN 24058963
Kamath, GM and Sundaram, Ramesh and Gupta, Nitesh and Subbarao, M (2007) Health monitoring of composites aircraft structures using fibre optic sensors: Some issues and challenges. In: Proceedings of the National Seminar on Aerospace Structures, 15-16 Oct 2007, BITS, Pilani.
Kanagarajan, V (1977) Aerodynamics performance of the wing with leading edge strakes. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kanagarajan, V (1976) Experimental studies on a wing with strake. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kanagarajan, V and Arokkiaswamy, A (1986) Experimental Studies on a 1/12 Scale Model of Prithvi Missile. Project Report. NAL, Bangalore.
Kanagarajan, V and Hartmann, K (1988) Force Measurements on a Body wing tail configuration (KaHa Model) at Mach numbers of 0.4 , 0.6 and 0.8 and incidences from 30° to 65°. Project Report. National Aerospace Laboratories, Bangalore.
Kanakamuthu, and Chandra, AP and Ashoka, BS and Majhi, Samay and Jayaraman, M and Kumar, VS and Seenappa, and De, Manabendra M and Manjunath, MR and Isaac, JJ (2011) Field trials of the NMITLI 500 kW Horizontal-Axis Wind Turbine System. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kanakamuthu, and Rajeev, KT and Chandra, AP and De, Manabendra M (2011) Aerodynamic design of the 500 W wind turbine rotor/blade. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kangovi, S (1977) Review of base row studies with particular emphasis on Chapman-Korst analysis. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kangovi, S and Krishnan, V (1982) Measurements related to afterbody studies on thrust-minus-drag rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kangovi, S and Page, RH (1978) Subsonic turbulent flow past a downstream facing annular step. In: Winter Annual Meeting on American Society of Mechanical Engineers, 10-15 Dec 1978, California, USA.
Kangovi, S and Page, RH (1977) The turbulent flow through a sudden enlargement at subsonic speeds. In: 6th Conference on Australian Hydraulics and Fluid Mechanics, 5-9 Dec 1977, Adelaide, Australia.
Kannan, TS and Saravana, BV (1980) Design and fabrication of a laboratory scale tape coating unit. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kapadi, Yogesh and Pashilkar, AA (2005) Aero-Thermodynamic Model for Digital Simulation of Turbofan Engine. Project Report. National Aerospace Laboratories, Bangalore.
Kariappa, - (1968) Kinametically consistent unsteady aerodynamic coefficients13; in supersonic flow Part I : Theoretical basis. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Karthikeyan, N and Ashwin Kumar, S and Venkatakrishnan, L (2013) Correlation Studies in the Acoustic Far-Field of Non-ideally Expanded Supersonic Jets. In: 19th AIAA/CEAS Aeroacoustics Conference , 25 May 2013, Berlin, Germany.
Karthikeyan, N and Sudhakar, S and Suriyanarayanan, P (2014) Experimental Studies on the effect of Leading edge Tubercles on Laminar Separation Bubble. In: AIAA SciTech 2014, 13 Jan 2014, National Harbor, Maryland, USA.
Karthikeyan, N and Venkatakrishnan, L (2010) Application of photogrammetry to surface flow visualization. Experiments in Fluids, 49 (9). pp. 1-10. ISSN 0723-4864
Karthikeyan, N and Venkatakrishnan, L (2015) Flow field and acoustic investigations of the launch vehicle environment during lift-off. In: 21st AIAA/CEAS Aeroacoustics Conference, AIAA AVIATION Forum, 22-26 June 2015, Dallas, TX.
Kashyap, SK (2003) Automated process noise covariance computation. Technical Report. National Aerospace Laboratories, Bangalore, India.
Khadeeja Nusrath, TK and Kaliyari, D and Singh, Jatinder and Patel, V V (2016) Enhancing real time monitoring support for safe envelope expansion. IFAC-PapersOnLine, 49 (1). pp. 254-259. ISSN 24058963
Khan, AA and Venkat Iyengar, S (2009) Numerical simulation of supersonic combustion of hydrogen in a vitiated air stream. In: 11th AeSI Annual CFD Symposium, 11-12 Aug 2009, Inidian Institute of Science, Bangalore, India.
Khare, Alok and Madhuranath, Padma (1993) Linear simulation software LINSIM. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Khatri, AK and Sinha, NK (2013) Accessible regions for controlled aircraft maneuvering. Journal of Guidance, Control and Dynamics, 36 (6). pp. 1829-1834. ISSN 0731-5090
Khatri, AK and Kumar, Vineet (2016) Bifurcation analysis of a generic pusher type transport aircraft configuration in near-stall flight. In: 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016, 25-30 September 2016, Korea.
Kidambi, R and Deshpande, MD (2000) Liquid Sloshing in 2 -Dimensional Rectangular Containers. Project Report. National Aerospace Laboratories, Bangalore, India.
Kishor Kumar, and Senthil Kumaran, R and Swamy, KMM and Jagannatha Rao, B and Krishnoji Rao, NS and Poornima, N and Loganathan, KS (2010) Aerodynamic Investigations on a Single Stage Turbine to Benchmark LSRR. Project Report. CSIR-NAL, Bangalore, Bangalore, INDIA.
Kishore, Kumar S and William, T and Laynet, W (1988) Magnetohydrodynamic flow and heat transfer about a rotating disk with suction and injection at the disk surface. Computers and Fluids, Vol. 1 ( 2). pp. 183-193. ISSN 0045-7930
Kressel, I and Dorfman, B and Botsev, Y and Handelman, A and Balter, J and Pillai, ACR and Prasad, MH and Gupta, Nitesh and Joseph, AM and Sundaram, Ramesh and Tur, M (2015) Flight validation of an embedded structural health monitoring system for an unmanned aerial vehicle. Smart Materials and Structures, 24 (7). pp. 1-10. ISSN 0964-1726
Krishnamoorthy, V and Pai, BR and Paranjpe, PA (1978) Heat transfer in turbine cascades - An experimental and analytical study. In: 4th Conference on National Heat and Mass Transfer, 21-23 Nov 1978, Roorkee, India.
Krishnamoorthy, V and Pai, BR and Sukhatme, SP (1987) Influence of upstream flow conditions on the heat transfer to nozzle guide vanes. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Krishnamurthy, K (1989) Tests on NAL-114-26-00 symmetric supercritical airfoil in 0.3M Wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Krishnamurthy, K and Wulff, G (1993) DIVA on PC Part 1: Analysis of time-dependent data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Krishnamurthy, M and Venugopal, S (1991) Correlation study of the wing-body interference factor for high angles of attack. Journal of Aeronautical Society of India, 43 (2). pp. 93-99.
Krishnan, AG and Rajeswari, Ramamurthy S (2009) Database management system for SARAS Wind Tunnel Data. In: National Conference on Wind Tunnel Testing 2009-CP9, 12-14 Mar 2009, IISc., Bangalore.
Krishnan, V (1989) Study of the turbulent boundary layer on an afterbody. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Krishnan, V and Kangovi, S (1980) Calibration of six-component internal strain gage balance. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Krishnan, V and Mathur, NB (1997) Afterbody Boundary Layer Measurements in the Base Flow Facility. Technical Report. National Aerospace Laboratories, Bangalore,India.
Krishnan, V and Mukund, R and Subaschandar, N (2000) Calibration Studies of NAL 1.5m Low Speed Wind Tunnel. Technical Report. National Aerospace Laboratories, Bangalore, India.
Krishnan, V and Shashikanth, BN and Mukund, R (1995) Experiments on Transition Detection Using chemical sublimation Technique and Hot-Film Gauges. Technical Report. National Aerospace Laboratories, Bangalore, India.
Krishnan, V and Viswanath, PR and Rudrakumar, S (1997) Effect of riblets on axisymmetric base pressure. Journal of Spacecraft and Rockets, 34 (2). pp. 256-258. ISSN 0022-4650
Krishnan , Anjana and Ananda, CM (2011) Validation of FCOM profiles for aircraft engine flight data using neural networks. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Krothapalli, A and Venkatakrishnan, L and Lourenco, L (2000) Crackle - A dominant component of supersonic jet mixing noise 13; 13;. In: AIAA/CEAS, Aeroacoustics Conference and Exhibit, 6th (21st AIAA Aeroacoustics Conference), 12-14 June 2000, Lahaina, United States.
Krothapalli, A and Venkatakrishnan, L and Lourenco, L and Elavarasan, R (2000) Supersonic jet noise suppression by water injection 13;. In: AIAA/CEAS, Aeroacoustics Conference and Exhibit, 6th (21st AIAA Aeroacoustics Conference), 12-14 June 2000, United States.
Krothapalli, A and Venkatakrishnan, L and Lourenco, L and Greska, B (2003) Turbulence and noise suppression of a high-speed jet by water injection. Journal of Fluid Mechanics, 491. pp. 131-159. ISSN 1469-7645
Kulkarni, DS and Raghavendra, B and Rajani, BN and Majumdar, Sekhar (2008) Performance analysis of eddy-viscosity based turbulence models for attached and separated flows. In: Proceedings of the 12th Asian Congress of Fluid Mechanics, 18-21 Aug 2008, Daejeon, Korea.
Kulkarni, DS and Sarkar, S and Majumdar, Sekhar (2007) Prediction of airfoil characteristics for a wide range of angle of attack using different turbulence models. In: Proceedings of the Indo-Australian workshop on CFD Approach on Fluid Flow, Heat and Mass Transfer and Symposium on CFD applications in Multidisciplinary Areas (IAWS-CFD 2007), 12-14 Apr 2007, Roorkee, India.
Kulkarni, DS and Sarkar, S and Rajani, BN and Majumdar, Sekhar (2007) Prediction of airfoil characteristics for a wide range of angle of attack using low REk- and v2-f turbulence models. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Kulkarni, DS and Rajani, BN (2021) Numerical Analysis of High Reynolds Number Effects on the Performance of GAW-1 Airfoil. In: Design and Development of Aerospace Vehicles and Propulsion Systems, Singapore.
Kulkarni, S and Satish Kumar, S and Santhosh Kumar, S and Sinha, UK and Shah, B and Satish Kumar, K and Steve Mithran, AJ and Monickavasagom Pillai, K (2021) Vibration Reduction in Indigenous Wankel Rotary Combustion Engine with Structured Layer Damping. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Kumar, A and Shankar, PN (1980) A potential flow model for lifting separated flows. In: ASME 1980, 10-13 Mar 1980, New Orleans, USA.
Kumar, Ajai (1972) A self - aligning probe traverse mechanism for turbomachinery (Design amp; Calibration). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kumar, Anand (1996) Accurate development of leading-edge vortex using an embedded conical grid. AIAA Journal, 34 (10). pp. 2038-2046. ISSN 0001-1452
Kumar, Anand (1996) Accurate development of leading-edge vortex using an embedded conical grid. AIAA Journal, 1 (3). pp. 1-9. ISSN 1081-0102
Kumar, Anand (1977) Eigenfunctions of the poiseuille flow development. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kumar, Anand (1993) Finite volume method using Runge-Kutta time-stepping for solution of Euler equations. In: CFD: Advances and Applications, 1993, India.
Kumar, Anand and Shankar, PN (1978) The wake source model for lifting separated flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kumar, Anand and Yajnik, KS (1976) Poiseuille flow development by eigenfunction expansion method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kumar, K and Nair, Manoj T (2007) Robust and fast algorithm to compute mesh deformations of multi-block structured grids. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Kumar, M and Arakeri, JH and Shankar, PN (1995) Translational velocity oscillations of piston generated vortex rings. Physics of Fluids, 7 (11). pp. 2751-2756.
Kumar, N and Nair, Manoj T (2013) Application of density corrected Spalart-Allmaras model to flow past ogive cylinder at high angles of attack. Journal of Applied Fluid Mechanics, 6 (3). pp. 375-384. ISSN 1735-3572
Kumar, R (2000) MAVs: A Brief Summary. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kumar, R and Viswanath, PR (2002) Passive control of surface pressure fluctuations in reattaching flows. Aeronautical Journal, 106 (1066). pp. 669-674.
Kumar, Rajan and Ali, Mohd Y and Alvi, Farukh and Venkatakrishnan, L (2011) Generation and control of oblique shocks using microjets. AIAA Journal, 49 (12). pp. 2751-2759. ISSN 0001-1452
Kumar, Rajeev and Sundaram, S (2000) Refurbishment and calibration studies of 0.3m water tunnel facility13; 13;. Technical Report. National Aerospace Laboratories, Bangalore, India.
Kumar, Siva K and Sharanappa, Sajjan V (2010) Numerical Simulation of Unsteady Flow over a Plunging Aerofoil Using an Implicit Reynolds Averaged Navier-Stokes Slover. Project Report. NAL, Bangalore.
Kumar, Sunil C (1989) Numerical solution of navier-stokes equations for two- dimensional viscous compressible flows. AIAA Journal, Vol. 2 (7). pp. 843-844. ISSN 0001-1452
Kumar, VA and Paranjpe, PA (1979) Experimental evaluation of damping coefficient of a squeeze film mounted ball bearing. In: 4th International Symposium on Air Breathing Engines, 1-6 Apr 1979, Florida, USA.
Kumar, Vineet and Kamaleshaiah, MS and Panda, GK and Mukund, R and Karthikeyan, N (2007) Wind tunnel measurements on powered model of SARAS aircraft to assess the effect of airframe-propeller flow interaction on propeller thrust. In: 3rd Symposium on Applied Aerodynamics and design of aerospace vehicle (SAROD-2007), 22-23 Nov 2007, Thiruvananthapuram, Kerala, India.
Kumar, AA and Onkar, AK (2021) Robust Flutter Prediction of an Airfoil Including Uncertainties. In: Design and Development of Aerospace Vehicles and Propulsion Systems, 15 June 2021, Singapore.
Kumar, S and Onkar, AK and Maligappa, M (2019) Frequency domain approach for probabilistic flutter analysis using stochastic finite elements. Meccanica, 54 (14). pp. 2207-2225. ISSN 00256455
Kumar, S S and Bhanudasji Alone, D and Thimmaiah, SM and Mudipalli, JRR and Kumar, L and Ganguli, Ranjan and Kandagal, SB and Jana, S (2021) Aerodynamic behavior of a transonic axial flow compressor stage with self-recirculating casing treatment. Aerospace Science and Technology, 112. ISSN 12709638
Kumar , R and Venkatakrishnan, L and Wiley, Alex and Alvi, Farukh (2010) Role of coherent structures in supersonic impinging jet noise and its control. In: 16th AIAA/CEAS Aeroacoustics Conference, 7-9 Jun 2010, Stockholm, Sweden.
Kumar P, Arun and Verma, SB and Elangovan, S (2011) Study of jets from rectangular nozzles with square grooves. Aeronautical Journal, 115 (1165). pp. 187-196. ISSN 0001-9240
Kumaran, RS and Alone, DB and Nassar, A and Kumar, P (2021) Preliminary aerodynamic design of A S-co2 axial turbine. In: Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021, December 2–3, 2021.
Kumari, Asha and Kotresh, Gaddikeri M and Byji, Varughese (2010) Stress Analysis of Ailerons-control bracket attachment to front-spar in SARAS composite wing. Project Report. NAL, Bangalore.
Kumari, Asha and Kotresh, Gaddikeri M and Byji, Varughese (2010) Stress Analysis of Composite wing of SARAS Aircraft at extreme operating temperatures. Project Report. NAL, Bangalore.
Kumari, Asha and Murali Krishna, D and Kotresh, Gaddikeri M and Byji, Varughese (2010) Local 3-D stress analysis of metallic front and rear landing gear beams of SARAS-composite wing. Project Report. NAL, Bangalore.
Kurade, RB and Venkatakrishnan, L and Jagadeesh, G (2021) Control of shock-induced vortex breakdown on a delta-wing-body configuration in the transonic regime. Aeronautical Journal, 126 (1299). 768 -792. ISSN 00019240
Lakshminarayana, HV (1976) Finite element analysis of laminated composite shell junctions. Computers and Structures, 6 (1). pp. 11-15.
Lakshminarayana, HV and Godbole, AK (1974) Finite element analysis of laminated anisotropic shell structures. In: Seminar on the Role of Computers in Structural Analysis, Design and Optimisation, 13-14 June 1974, Bangalore, India.
Lakshminarayana, HV and Mahishi, JM and Aruna, HM (1979) On the behaviour of cracks in laminated composite panels. In: Proceedings of the International Conference on Fracture Mechanics in Engineering Application, 26-30 Mar 1979, Bangalore, India.
Lathasree, P (2009) Studies on optimal aviation fuel consumption-closing report. Technical Report. NAL.
Lathasree, P and kamali, C and Navendu, Kumar (2009) Modeling and simulation for LCA. Technical Report. NAL.
Leelavathi, K and Rajappa, N (1976) Operational validation of a computer program to calculate incompressible potential flow past a lifting airfoil by the method of catherall foster and sells. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Lokhandwala, OA (1977) Studies of 'N' waves and weak shock waves in the 75 x 100 mm NAL shock tube. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Lokhandwala, OA (1977) Studies of Nquot;waves and weak shock waves in the 75x100 mm shock tube. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Madhava Rao, C and Raj Mahindra, and Nagaraj Rao, TG (1992) Light transport aircraft - an integrated approach to aircraft manufacture and overhaul facility. Project Report. National Aerospace Laboratories, Bangalore.
Madhavan, KT (2001) Phase-Averaged LDV measurements in a bluff-body wake. Technical Report. National Aerospace Laboratories, Bangalore, India.
Madhavan, KT and Mukund, R (2009) High-speed flow visualisation using shear-sensitive liquid crystals. In: National Conference on Wind Tunnel Testing 2009-CP12, 12-14 Mar 2009, IISc., Bangalore.
Madhavan, KT and Ramesh, G (1993) LDV measurements in turbulent jet and separated flows. Project Report. National Aerospace Laboratories, Bangalore.
Madhavan, KT and Sajeer, Ahmed and Suriyanarayanan, P and Ramesh, G CALIBRATION OF 0.55m LOW SPEED WIND TUNNEL FOR LOW REYNOLDS NUMBER STUDIES. In: National Conference on Windtunnel Testing, July 12-14, 2007 , IIT Kanpur.
Madhuranath, Padma and Lathasree, P (1993) Scheduling of control surfaces for aircraft performance optimisation. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.
Madhuranath, Padma and Sridhar, JK and Srinatha Sastry, CV (1989) Flight Simulation of HS - 748 with and without rotodome Part 3- Aerostatic Model Formulation. Project Report. NAL, Bangalore.
Mahadevan, Srikrishna and Kutlu, BF and Golsen, MJ and Verma, SB (2015) Experimental study of unsteady wake effect on a film-cooled pitchwise-curved surface. International Journal of Heat and Mass Transfer, 83. pp. 118-135. ISSN 0017-9310
Mahadevan, Sudha and Giridhar, A (1992) Floppy to rigid transition and chemical ordering in Ge-Sb(As)-Se glasses. Journal of Non-Crystalline Solids, 143 (1). pp. 52-58.
Mahalingam, V and Srikantan, KV and Balakrishna, S (1975) Modification of the model incidence control system of the NAL 4-ft. trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mahalingam, V and Srikantan, KV and Mahalingam, R and Nagabhushana, S and Krishnamurthy, DR and Raghumurthy, G (1976) Redesign of the memory in digital data acquisition system of the NAL 4-Ft. trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Majeed, M and Kar, IN (2013) Design and convergence analysis of stochastic frequency estimator using contraction theory. IET Signal Process, 7 (5). pp. 389-399. ISSN 1751-9675
Majeed, M and Singh, Jatinder and Kar, IN (2012) Identification of aerodynamic derivatives of a flexible aircraft. Journal of Aircraft, 49 (2). pp. 654-658. ISSN 0021-8669
Majumdar, Sekhar (1993) Finite volume method for computation of viscous flow in complex configurations. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R Narasimha on his 60th Birthday, 1993, Sikkim.
Majumdar, Sekhar and Deshpande, MD (1994) CFD: Advances and applications. In: UNI series program entitled 'CFD - Advances and Applications', 26-28 Oct 1994, Bangalore, India.
Majumdar, Sekhar and Godbole, AK and Sridhar, S and Govindarajan, Rama and Ramachandran, J and Punekar, J (1990) A Computer Code for Calculation of Two Dimensional Incompressible Turbulent Recirculating Flows with Complex13; Irregular Boundaries. Technical Report. National Aerospace Laboratories, Bangalore, India.
Majumdar, Sekhar and Sinha, UN Development of a Finite Volume Algorithm for Calculation of Three Dimensional Incompressible Turbulent Recirculating Flows. Project Report. NAL, Bangalore.
Mallikarjuna, HV (1987) Testing of Automatic Inflatable Life Jacket in Open Jet Facility Phase II. Project Report. National Aerospace Laboratories, Bangalore.
Mallikarjuna, HV (1987) Wind tunnel tests on 1 /6th scale model of pilotless target aircraft configuration - 4. Project Report. National Aerospace Laboratories, Bangalore.
Mandal, AC and Venkatakrishnan, L and Dey, J (2010) A study on boundary-layer transition induced by free-stream turbulence. Journal of Fluid Mechanics, 660. pp. 114-146. ISSN 0022-1120
Mani, A and Vedavathi, BM and Vijayan, Kalyani (1982) Crystal data on the radioprotectants,N-(2-Mercaptoprofionyl13; ) cycline and N.N.N',N',-Tetramethyl-1,4-Phenylene diamine-dihydrochloride. Current Science, 51 (4). p. 192.
Manickam, MD (1987) A research facility for film cooling investigations with emphasis on the instrumentation system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Manickam, MD and Mahalingam, S (1973) Performance of a cobra probe and an asymmetric probe in a cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Manickam, MD and Mahalingam, S and Murugesan, K (1975) Choice of blade chord, pitch and height based on secondary flow losses. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Manickam, MD and Murugesan, K (1978) Calibration characteristics of various types of two dimensional yaw probes,used in cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Manickam, MD and Murugesan, K (1989) Effect of discrete hole film injection on aerodynamic performance of a turbine cascade. In: 9th International Symposium on Air Breathing Engines, Sep 1989, Athens, Greece.
Manisankar, C and Sajeer, Ahmed and Thiagarajan, V (2010) Investigation of starting process of a movable intake configuration at high supersonic speeds. In: Proceedings of the 13th Asian Congress of Fluid Mechanics, 17-21 Dec 2010, Dhaka, Bangladesh.
Manisankar, C and Verma, SB (2015) Parametric Study on Steady Micro-Jet Actuators for Control of Unsteady Shock Motion in a Compression Induced Interaction at Mach 2.0. In: 7th Symposium on Applied Aerodynamics And Design of Aerospace Vehicles (SAROD-2015) , 03-12-2015, Vikram Sarabhai Space Centre, Trivandrum.
Manisankar, C and Verma, SB and Raju, Channa (2012) Shock-wave boundary-layer interaction study on a compression corner using pressure-sensitive paint. International Journal of Aerospace Innovations, 4 (1-2). pp. 29-39. ISSN 1757-2258
Manisankar, C and Verma, SB (2021) Assessment of Flow Field Behind the Mechanical Vortex Generators at Mach 2.0. In: Proceedings of 16th Asian Congress of Fluid Mechanics, Singapore.
Manjuprasad, M and Sathish, B S and Viswanath, S (2007) Dynamic aeroelastic subsonic discrete gust response analysis of lifting surfaces in time domain using Newark's method. Technical Report. National Aerospace Laboratories, Bangalore, India.
Manoharan, LC and Muthuvel, S and Seshadri, K and Diwakar, Philipm (1990) Fiberoptic air data system. In: 17th ICAS, Congress, 9-14 Sept 1990, Stockholm, Sweden.
Mathur, JS and Chakrabartty, SK (1994) Approximate factorization scheme for elliptic grid generation with control functions. Numerical Methods for Partial Differential Equations, 10 (6). pp. 703-713.
Mathur, JS and Rajani, BN and Kulkarni, DS and Subrahmanya, MB (2009) Computational Fluid Dynamics Applications to MAVs. In: MAV Workshop- Challenges and Presferred Outcomes, 13 November 2008, National Aerospace Laboratories.
Mathur, JS and Srinivasa, C (1988) Solution of a second order ODE by a multigrid method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mathur, NB (1998) Correlation for the Estimation of Afterbody Drag with Hot Jet Exhaust. Journal of Aircraft, 35 (6). pp. 981-984.
Mathur, NB (1991) Development of underexpanded sonic jet exhausting from the convergent nozzle of an axisymmetric afterbody configuration. In: International Symposium on Air Breathing Engines, 1-6 Sep 1991, Nottingham, England.
Mathur, NB (1984) Effects of under expanded jet on afterbody drag of an axisymmetric configuration. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mathur, NB and Mohan, Jai and Lokhandwala, OA (1978) Cold jet simulation RIG for the NAL 1.2M trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mathur, NB and Rajeev, Kumar (2004) Experimental Studies on 1/15th Scale SARAS Afterbody Model with Underside Fuselage Fairing, Ventral Fins, Nacelles and Stub Main Wing. Technical Report. National Aerospace Laboratories, Bangalore, India.
Mathur, NB and Ramakrishnan, MS (1984) A rig for testing afterbodies of aerospace vehicles in presence of j e t in 0.3m trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Mathur, NB and Viji, M (2009) Experimental Studies on Twin Jet Afterbody-Nozzles System of Combat Aircraft Configuration. Project Report. National Aerospace Laboratories, Bangalore.
Mathur, NB and Viji, M (2010) Experimental studies on twinjet afterbody-nozzle system of combat aircraft configurations. Project Report. National Aerospace Laboratories, Bangalore.
Mathur, NB and Viji, M (2008) Measurements of aerodynamic loads on afterbody-nozzle configuration of HSTDV-SERN nozzle system. Project Report. National Aerospace Laboratories, Bangalore.
Mathur, NB and Viswanath, PR (2004) Drag Reduction from Square-Base Afterbodies at High Speeds. Journal of Aircraft, 41 (4). pp. 811-820.
Mathur, NB and Yajnik, KS (1989) Axisymmetric afterbody flow separation at transonic speeds in presence of jet exhaust. In: 9th International Symposium on Air Breathing Engines, 03-08 Sept 1989, Athens, Greece.
Mathur, NB and Yajnik, KS (1985) Jet plume temperature effects on afterbody pressure distribution and drag. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mathur, NB and Yajnik, KS (1985) Jet plume temperature effects on afterbody pressure distribution and drag. In: 7th International Symposium on Air Breathing Engines, 2-6 Sep 1985, Beijing, China.
Mathur, NB and Yajnik, KS (1990) Underexpanded jet-freestream interactions on an axisymmetric afterbody configuration. AIAA Journal, 28 (1). pp. 47-50. ISSN 0001-1452
Mayuresh, - and Sudhakar, S and Ramesh, G and Sajeer, Ahmed Calibration of 0.2m low speed wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Merchant, Laxmikant and Ahmed, Sajeer (2003) Investigation of Methods for the Alleviation of Supersonic Flow-Instability of a Pitot Air-intake. Project Report. National Aerospace Laboratories, Bangalore.
Mohamed, Majeed and Dongare, V (2021) Identification of a Flexible Aircraft Derivatives. In: Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation. SpringerBriefs in Applied Sciences and Technology . Springer, Singapore, pp. 47-58. ISBN 978-981-16-0103-3
Mohamed, Majeed and Dongare, V (2021) Neural Modeling and Parameter Estimation. In: Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation. SpringerBriefs in Applied Sciences and Technology . Springer Science and Business Media Deutschland GmbH, Singapore, pp. 13-19. ISBN 978-981-16-0103-3
Mohamed, Majeed and Gopakumar, M (2021) Design of sliding mode flight control system for a flexible aircraft. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 236 (9). ISSN 09544100
Mohamed, Majeed and Joy, N (2021) Lateral directional aircraft aerodynamic parameter estimation using adaptive stochastic nonlinear filter. Aeronautical Journal, 125 (1294). 2217 -2228. ISSN 00019240
Mohan, Jai (1977) A study of techniques for generating store separation data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mohan, KH (1989) Fabrication of 1/20th scale wind tunnel model of jaguar aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Mohan, SR and Srinivas, K (1980) Computation of response times of pressure measuring systems employing narrow bore tubing. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mohan Ram, VS and Shyam, Chetty (1983) Estimation of lift and moment coefficients for a closed coupled canard model using datcom methods. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Mozumdar, S and Patel, TS (1980) Investigation on rotating ailerons. Aeronautical Society of India, Journal, 32. pp. 1-5.
Mudkavi, Vidyadhar Y (1993) The phenomenon of vortex breakdown. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.
Mudkavi, Vidyadhar Y and Suryanarayana, GK and Thangavelu, RP (2009) Aerodynamic data sharing and database: A proposal. In: National Conference on Wind Tunnel Testing 2009-CP16, 12-14 Mar 2009, IISc., Bangalore.
Mukund, R (2002) Calculation of relaminarizing flow using the quasi-laminar equations. Project Report. National Aerospace Laboratories, Bangalore, India.
Mukund, R (2009) Overview of the experimental facilities at the Experimental Aerodynamics Division, NAL. In: National Conference on Wind Tunnel Testing (2009-IT7), 12-14 Mar 2009, IISc., Bangalore.
Mukund, R (2002) Relaminarization in a short acceleration zone on a convex surface (NAL PD EA 0511). ["eprint_fieldopt_thesis_type_phd" not defined] thesis, Indian Institute of Science.
Mukund, R and Arivoli, D and Chandan Kumar, A (2009) Pressure measurement on NASA 0416 and NAL 7025 airfoils in the 1.5m wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Chandan Kumar, A (2014) Effect of MAV configuration on flow and performance. Technical Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Chandan Kumar, A (2010) Experiments on NAL 21463 airfoil in the 1.5m wind tunnel for NAL RTA. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Chandan Kumar, R (2013) Hot-wire measurements behind a propeller model. In: The Third National Conference on Wind Tunnel Testing , 2013-08-23, VSSC, Trivandrum.
Mukund, R and Kamaleshaiah, MS (2004) Force measurement in the 1.5m tunnel on the SARAS aircraft model with powered propellers. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Karthikeyan, N Experimental investigations and evaluation of MAV planforms. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Karthikeyan, N (2009) Wind Tunnel Measurements on MAV Planforms. In: MAV Workshop Challenges and Preferred Outcomes, 13 November 2008, National Aerospace Laboratories.
Mukund, R and Madhavan, KT and Venkatakrishnan, L (2007) Study of Dynamic Stall on an Oscillating Airfoil using Particle Image Velocimetry. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Viswanath, PR (2006) Experimental data on relaminarising boundary layers on convex and flat surfaces. Project Report. National Aerospace Laboratories, Bangalore, India.
Mukund, R and Viswanath, PR and Prabhu, A and Vasudevan, B (2003) Study of glancing and blunt fin shock-boundary layer interactions at low supersonic mach numbers. Project Report. National Aerospace Laboratories, Bangalore.
Murthy, AV (1974) Hypersonic flow over blunted slender wedges. Journal of Aircraft, 11. pp. 649-651. ISSN 0021-8669
Murthy, AV (1975) Hypersonic flow over concave surfaces with leading-edge bluntness. AIAA Journal, 13 (9). pp. 1230-1233. ISSN 0001-1452
Murthy, AV and Hebbar, KS (1974) Calculation of laminar boundary layers on continuous surfaces by Meksyn's method. AIAA Journal, 12 (5). pp. 732-733. ISSN 0001-1452
Murthy, AV and Rao, DM (1975) Pilot ludwieg tube project. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Murthy, HS and Suryanarayana, GK (1986) Wind Tunnel Simulation of ASLV Strap-on Booster Separation Trajectory (Phase III). Project Report. NAL, Bangalore.
Murthy, MVA and Muralikrishna, Radha V (1998) TURBOPLOT-Post processor graphics software for CFD analysis of turbomachines. Technical Report. National Aerospace Laboratories, Bangalore, India.
Murthy, MVA and Paranjpe, PA (1977) Test facility for performance evaluation of model turbine stages. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Murthy, MVA and Paranjpe, PA (1977) Turbine test facility of Propulsion Division. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Murthy, MVV (1967) Stresses around an elliptic hole in a cylindrical shell. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Murthy, MVV and Raju, KN and Viswanath, S (1979) On the bending stress distribution at the tip of a stationary crack from Reissner's theory. In: Proceedings of the International Conference on Fracture Mechanics in Engineering Application, 26-30 Mar 1979, Bangalore, India.
Murthy, MVV and Viswanath, S and Rao, krishna Murty (1988) Two-dimensional model for crack closure effect in plates under bending 13; 13;. Engineering Fracture Mechanics, 29 (4). pp. 435-452. ISSN 0013-7944
Murthy, Onkar and Munirudrappa, N and Srikanth, L and Rao, RMVGK (2006) Strength and stiffness optimization studies on honeycomb core sandwich panels13;. Journal of Reinforced Plastics and Composites, 25 (6). pp. 663-671.
Murthy, SNB (1965) Acoustic oscillations non-adiabatic flow systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Murthy, Sundara H and Suryanarayana, GK and Lochan, R and Pandian, S and Sivaramakrishnan, AE (1995) Wind tunnel simulation of multibooster separation trajectories of a launch vehicle13;. Journal of spacecraft and Rockets, 32 (3). pp. 561-563. ISSN 0022-4650
Murugesan, K (1978) Analysis of prancis turbine runner blade channel flow. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Murugesan, K and Sankaranarayanan, S and Ramasastry, S (1975) Performance evaluation of a cold-air turning. Technical Report. National Aeronautical Laboratory, Bangalore, India.
NAL, (1990) Eighth Five Year Plan Proposals (1990-1995). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nagabhushana, S and Krishnan, A (1965) Temporary storage check unit for NAL data system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nagapurwala, QH and Girigoswami, H and Mohan, K (1987) Effect of variable geometry inlet guide vanes on the performance of a high speed compressor stage. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Nagarajan, V and Sundaramurthy, H (1982) Estimation of inertial peoperties of wind tunnel aircraft models Part I: Development of a computer programme13; Part II: Description of a rig and measurements on typical models. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nagarajan, V and Sundaramurthy, H (1988) Estimation of stability derivatives and dynamic stability characteristics of basic and AEW HS-748 aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Nagpurwala, QH (1989) Software modules for analysing and plotting the probe calibration data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nagpurwala, QH and Mohan, K (1974) Proposed instrumentation for compressor research rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Naidu, P and Girija, G and Raol, JR (2005) Target Tracking and Fusion Using Imaging Sensor and Ground Based Radar Data 2005-5842. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, 15-18 August 2005, San Francisco, California.
Nair, Manoj T and Saxena, SK and Naresh, Kumar (2004) Implementation and Testing of New Upwind Schemes in a Multi-block Code. Project Report. National Aerospace Laboratories, Bangalore, India.
Nair, RU and Jha, RM (2004) Tuning of EM performance for streamlined aircraft radomes13;. IEEE Antennas and Propagation Society, 1 (--). pp. 874-877.
Nandanan, M and Ramaswamy, MA (1986) Aerodynamic characteristics of lifting symmetric supercritical airfoils. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nandanan, M and Ramaswamy, MA (1985) Design of lifting symmetric supercritical airfoils. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nandanan, M and Ramaswamy, MA (1987) Lifting symmetric supercritical airfoils for wing design of combat aircraft 13; 13;. Communications in Applied Numerical Methods, Vol. 3. pp. 463-468. ISSN 0748-8025
Nandanan, M and Ramaswamy, MA (1985) Supercritical wing design for combat aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nandanan, M and Shantha Kumari, S (1987) Development of a Computer-Code for Viscous-Inviscid Analysis of Transonic Flow past Airfoils and Wings including Shock-wave Boundary Layer Interactions - Closure Report for ARDB project AE-O-147. Project Report. National Aerospace Laboratories, Bangalore.
Narasimha, R (1989) Turbulence at the CrossRoads : The Utility and13; Drawbacks of Traditional Approaches. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narasimha, R (1989) Turbulence at the cross roads: The utility and drawbacks of13; traditional approaches. In: Workshop on Turbulence at the Cross Roads, or Whither Turbulence?, 22-24 Mar 1989, Ithaca, NY.
Narasimha, R (1993) Turbulence on computers. Current Science, 64 (1). pp. 28-32.
Narasimha, R (1991) The dynamics of the transition zone and its modeling. In: VKI, Boundary Layers in Turbomachines 100 p (SEE N92-24336 15-07) 1991, Belgium.
Narasimha, R and Das, P (1986) Infinitely strong shock. In: 15th International Symposium on Rarefield Gas Dynamics, 16-20 Jun 1986, Grado, Italy.
Narasimha, R and Das, P (1986) The infinitely strong shock. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narasimha, R and Kumar, Kishore S (1986) The lift on an airfoil in a turbulent boundary layer 11. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narasimhan, SV and Harish, M (2004) Spectral estimation based on subband decomposition by harmonic wavelet transform and modified group delay13;. In: 2004 International Conference on Signal Processing and Communications, 11-14 Dec 2004.
Narasimhan, SV and Kumar, BKS (2004) Harmonic wavelet transform signal decomposition and modified group delay for improved Wigner-Ville distribution13;. In: 2004 International Conference on Signal Processing and Communications (SPCOM), 2004, Bangalore, India.
Narasimhan, SV and Pavanalatha, S (2003) Estimation of evolutionary spectrum based on STFT and modified group delay. In: IEEE TENCON 2003: Conference on Convergent Technologies for the Asia-Pacific Region, 15-17 Oct 2003, Bangalore, India.
Narayan, G (1988) Augmentation of instrumentation systems for 1.2m tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, G and Mahalingam, V and Rajagopalan, E and Seshadri, SN (1985) Data Acquisition Processing and Interactive Control Systems (DAPICS) : An Evaluation of various Offers. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, G and Mahalingam, V and Srikantan, KV (1975) Pressure sweep generator for the NAL 4-ft trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayan, G and Mahalingam, V and Srikantan, KV and Mahalingam, R (1976) Receiver oscillation studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayan, G and Mahalingam, V and Srikanthan, KV (1975) Presure sweep generator for the NAL 4-ft trisonic wind tunnel. Technical Report. National Aerospace Laboratories, Bangalore,India.
Narayan, G and Shiela, Srinivasan (1987) A closed loop control system for the forced oscillation mechanism for Pitch-yaw derivatives. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY (1988) Effect of Canard on the Characteristics of a 65° Delta Wing-A Preliminary Analysis of Experimental Data. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY and Gopinath, N (1986) Wind tunnel tests on lca delta-5 configuration part II: results at supersonic speeds and analysis. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY and Gopinath, N and Seshadri, SN (1985) Wind tunnel tests on MiG-2114 aircraft model with combat flaps. Project Report. NAL, Bangalore.
Narayan, KY and Gopinath, N and Seshagiri, SN (1988) Wind tunnel tests on LCA 6.12 configuration. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY and Hartmann, K (1988) Transonic and supersonic flow past a 65xB0; delta wing with rounded leading edges - analysis of experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayan, KY and Seshadri, SN (1985) Parametric analysis of combat aircraft performance requirements. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayan, KY and Seshadri, SN (1988) Vortical flows on the lee surface of delta wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayan, G and Mahalingam, V and Srikanthan, SG (1975) Pressure sweep generator for the NAL4-ft trisonic wind tunnel. Technical Report. National Aerospace Laboratories, Bangalore, India.
Narayana, CL and Ramamoorthy, P (1993) MULTHOPP - A PC-based software package for obtaining wing loads. Technical Report. National Aerospace Laboratories, Bangalore, India.
Narayana, CL and Sinha, AK and Ramamoorthy, P (1976) Estimation of drag-divergence mach number for an airfoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayana Rao, CK (1992) Experimental investigation of ejectors as drives for a low speed tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Narayana Rao, CK (1987) Specification for a schileren system for the 0.6m transonic wind tunnel of the National aeronautical laboratory, Bangalore. Project Report. National Aerospace Laboratories, Bangalore.
Narayana Rao, CK and Gopinath, N (1987) Effect of protuberances on the aerodynamic characteristics of ASLV. Project Report. National Aerospace Laboratories, Bangalore.
Narayana Rao, CK and Krishna Murthy, M (1992) Wind tunnel test studies on 1/7 scale NALLA-1 model. Project Report. National Aerospace Laboratories, Bangalore.
Narayanamurthy, RS (1973) Determination of aerodynamic nozzle contours for transonic cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Narayanan, Sathia and Lakshmi, RV and Basu, Bharathibai J and Channa Raju, - and Venkatakrishnan, L (2013) Supersonic testing of NAL binary pressure sensitive paint. International Journal of Aerospace Innovations, 5 (1). pp. 1-10. ISSN 1757-2258
Narayanan, Sathia and Lakshmi, RV and Basu, Bharathibai J and Raju, Channa and Venkatakrishnan, L (2011) Supersonic testing of NAL binary pressure sensitive paint. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Natarajan, K and Murugan, JN and Sathiyavageeswaran, S and Venkatakrishnan, L (2021) Image-based analysis of interactions between a steady jet and an impulsively started jet. Journal of Spacecraft and Rockets, 58 (6). pp. 1671-1680. ISSN 00224650
Nath, B and Das, S and Prasad, JK (2009) Flow field study on a 65-deg blunted delta wing. In: National conference on wind tunnel testing, 12-14 March 2009, Bangalore.
Nayak, A and Das, D (2021) Experimental and numerical investigation of flow instability in a transient pipe flow. Journal of Fluid Mechanics, 920. pp. 1-23. ISSN 00221120
Nilakantan, P (1960) Criteria for selection of compressed air storage system for the trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nilakantan, P (1963) High-speed wind tunnels for aerospace research. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Nilavarasan, T and Joshi, GN and Misra, A and Manisankar, C and Verma, SB (2021) Topological modifications due to ramped vanes in a flare-induced shock–boundary layer interaction flowfield. Journal of Visualization, 24 (5). pp. 991-1010. ISSN 13438875
Nirmal, C and Maithi, SN and Padmavathi, T and Vanaja, A and Rao, RMVGK (2006) Studies on hydroxyl terminated polybutadiene toughened phenolic resin13;. High Performance Polymers, 18 (1). pp. 57-69.
Nitin, Khamesra and Karthik, N (2009) Conformatory tests on 1:50 scale PSLV_XL configuration. Technical Report. National Aerospace Laboratories, Bangalore, India.
Nitin, Khamesra and Srinivasan, N (2009) Wind tunnel tests on 1:50 scale GSLV Mk II configuration. Technical Report. National Aerospace Laboratories, Bangalore, India.
Onkar, AK (2021) A successive robust flutter prediction technique for aeroelastic systems using µ method. Meccanica, 56 (10). pp. 2613-2629. ISSN 00256455
Padmarajaiah, SK and Ramaswamy, SK and Ramaswamy, A (2006) A beam and arch action model for computing the shear strength of prestressed and reinforced HSFRC beams. Journal of Structural Engineering, 28 (1).
Pai, BR and Abbey, DK (1981) Development of gas operating on sludge gas: Test results of modified dart 514/7 combustor studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Pandit, CM (1961) A note on the control system for the pressure regulating valve of blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Pankaj, AC and Shivaprasad, MV and Shantini, G and Chandra, N and Nandan , A M and Manjuprasad, M (2011) Flutter prediction of a swept back plate using experimental model parameters. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Parameswaraiah, R and Sankaranarayanan, PE (1966) Strain indicator. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Parameswaraiah, R and Sreeharamurthy, V (1972) Sound state constant temperature anemometer for fluid flow studies. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Parameswaran, V and Jategaonkar, RV (2001) Calibration of 5 - Hole Probe for Flow Angles from ATTAS Flight Data. Technical Report. National Aerospace Laboratories, Bangalore, india.
Parameswaran, V and Mary Preena, M (1998) Recursive Estimation of Model Error for Identifi- cation of Non-Linear Continuous Time Systems. Technical Report. National Aerospace Laboratories, Bangalore, India.
Parameswaran, V and Raol, JR and Madhuranath, Padma (1993) Mathematical model building from flight data for simulation validation of a modified aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Paranjpe, PA and Murugesan, K (1974) Role of machinery centre for power sector. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Pashilkar, AA (2003) FAST user's manual version 0.1. Technical Report. National Aerospace Laboratories, Bangalore, India.
Pashilkar, AA (2009) Model Based Design of Aerospace Control Systems. In: International Symposium on Opportunities and Challenges Facing Aviation inustry in Indian Subcontinent, 18-20, 2009, Sreenidhi Institute of Science and Technology, Hyderabad.
Pashilkar, AA (2003) SARAS rigid response to turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.
Pashilkar, AA (2001) Unsteady aerodynamic modeling at high incidence for flight dynamic analysis. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 6-9 Aug 2001, Canada, United States.
Pashilkar, AA and Kamali, C and Raol, JR (2007) Direct estimation of nonlinear aerodynamic coefficients. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 20-23 Aug 2007, Soutli Carolina, USA.
Pashilkar, AA and Sara, FA (1995) Landing Gear Modelling for Flight Simulation Part I. Technical Report. National Aerospace Laboratories, Bangalore, India.
Patil, SR (1994) Buffet tests on 1/20 scale lca model with leading edge slats at transonic speeds. Project Report. National Aerospace Laboratories, Bangalore.
Patil, SR and Raman, KS and Ramaswamy, MA (1986) Analysis of a special short wind tunnel internal strain gauge balance and comparison with experimental calibration data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Patil, SR and Raman, KS and Ramaswamy, MA (1986) Development of Experimental Techniques to Determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward -Flight - Progress Report for 1985-86. Project Report. NAL, Bangalore.
Patil, SR and Ramaswamy, MA (1987) Development of Experimental Techniques to Determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Progress Report for 1986-87. Project Report. National Aerospace Laboratories, Bangalore.
Patil, SR and Ramaswamy, MA (1988) Development of Experimental Techniques to determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Closure Report for AR & DB Project AE-0-154. Project Report. National Aerospace Laboratories, Bangalore.
Patil, SR and Ramaswamy, MA (1988) Development of experimental techniques for helicopter rotor performance studies. Aeronautical Society of India, Vol. 4 (3). pp. 201-209.
Patil, SR and Ramaswamy, MA (1987) Model helicopter rotor rig and associated strain gauge balance for performance studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Patil, SR and Sridharan, R (1989) Wind tunnel wall corrections to experimental data on wing-body combinations at high angles of attack. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Pavan, RMV and Saravanan, V and Dinesh, AR and Rao, YJ and Srihari, Shylaja and Revathi, A (2006) Hygrothermal effects on painted and unpainted glass/epoxy composites - Part A: Moisture absorption characteristics. Journal of Reinforced Plastics and Composites, 20 (12). pp. 1036-1047.
Poornima, N and Senthil Kumaran, R and Kumar, K (2021) Stationary and Rotating Frame Instrumentation for Large Scale Rotating Rig. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Prabhu, Dinesh K (1994) Parabolized Navier-Stokes solution of supersonic/hypersonic flows. In: CFD: Advances and Applications, 1994.
Prabhu, KR (1976) Drag prediction methods for prelimanary design of an aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Prabhu, KR (1977) Problems encountered in wind tunnel testing of fighter type airplane models. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Prabhu, M and Kumar, RA and Gopikrishnan, TH and Deshpande, PJ and Anandhakrishnan, U and Kiran, AS and Govindu, RP (2020) Rankine vortex formation during draining: A new twin port suppression strategy. Journal of Applied Fluid Mechanics, 13 (1). pp. 147-160. ISSN 17353572
Pradyumna simha, R and Janardan, BA and Krishnamurthy, V (1969) Flame stabilization by opposed jets. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Prakash, S and Kailash, K and Venkatanarayana, AR (1989) Design of a free standing tower for SAMIRA windmill. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Prakash, S and Tewari, SK (1992) Preliminary studies on SAMIRA flap. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Prakash Rao, Y and Ramakrishnan, SV and Hebbar, KS (1980) A computer programme for reduction of incompressible two dimensional boundary layer data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Prasad, Simha DS and Subramanian, NR (1979) Computation of aerodynamic characteristics of finite wings in steady supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Prathap, Aparajit and Nandini, S and Majumdar, Sekhar (2000) Geometric Modelling of Complex Shaped Objects Using NURBS Methodology. Project Report. National Aerospace Laboratories, Bangalore,India.
Prathap, Gangan and Ramesh Babu, C (1987) Field-consistency and violent stress oscillations in the finite element method 13; 13;. International Journal for Numerical Methods in Engineering, 24. pp. 2017-2033.
Prathap, Gangan and Somashekar, BR (1988) FIELD- AND EDGE-CONSISTENCY SYNTHESIS OF A 4-NODE QUADRILATERAL PLATE BENDING ELEMENT. International Journal for Numerical Methods in Engineering, 26 (8). pp. 1693-1708.
Prathapanayaka, R and Vinod Kumar, N and Santhosh Kumar, S and Veera Sesha Kumar, C and Krishnamurthy, SJ (2014) Design and Development of Three-Bladed Propeller for Micro Air Vehicles. International journal of robotics and mechatronics, 1 (2). pp. 53-61.
Prathapanayaka, R and Vinodkumar, N and Krishnamurthy, SJ (2013) Design and development of three bladed propeller for micro air vehicles. In: 9th International Conference on Intelligent Unmanned Systems (ICIUS 2013), 25-27 September 2013, Jaipur, India.
Prathapanayaka, R and Vinodkumar, N and Krishnamurthy, SJ (2011) Design, Analysis, Fabrication and Testing of Mini Propeller for MAVs. In: 5th Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), Bangalore.
Premalatha, and Ramamoorthy, P (1993) Development of PC-based Aeronautical Software (AEROWARE) 13; 13;. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 1993, Sikkim, India.
Premalatha, - and Srilatha, KR and Mudkavi, Vidyadhar Y (2021) Analysis of Propeller by Panel Method for Transport Aircraft. In: Design and Development of Aerospace Vehicles and Propulsion Systems, 15 June 2021, Singapore.
Priya, P and Singh, Hema (2007) Studies of Methods of Discretization for CFD-CEM Applications. Project Report. CSIR-NAL, Bangalore, National Aerospace Laboratories.
Priya, P and Singh, Hema and Kulkarni, PS and Jha, RM (2008) Multidisciplinary Computational Aerospace Sciences (MCAS): Preliminary Studies on Source Panel Method. Project Report. CSIR-NAL, Bangalore, National Aerospace Laboratories.
Pureswaran, Shankar and Santhanam, A (1974) Instrumentation for fluidic temperature sensor. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Radhakrishna, SR and Joseph, KA (1988) Regauging of internal strain gauge balance supplied by T.E.M limited to H.A.L., bangalore engineering. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Krishnan, RV and Rangaraju, R and Parameswara, MA and Venkataswamy, MA (1989) Analysis of Compressor Blade Failure. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Krishnan, RV and Rangaraju, R and Venkataswamy, MA (1989) Analysis of cracking of H? Turbine Blades of an Aeroengine. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Krishnan, RV and Rangaraju, R and Venkataswamy, MA (1989) Failure analysis of components from the tailplane attachment area of an aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Krishnan, RV and Rangaraju, R and Venkataswamy, MA (1989) Fracture Analysis of TGB Bolts, from A Helicopter. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Krishnan, RV and Rangaraju, R and Venkataswamy, MA (1989) Investigation of aileron control cable failure of a Pushpak aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Radhakrishnan, S and Krishnan, RV and Rangaraju, R and Venkataswamy, MA (1989) Investigation of Failure of Differential Gears. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Radhakrishnan, S and Krishnan, RV and Rangaraju, R and Venkataswamy, MA (1989) Investigation of the fracture in the III stage compressor blades of an Aeroengine. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Krishnan, RV (1989) Analysis Of fracture in a Kaplan turbine vane. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Krishnan, RV (1989) Report on the Failure of a Turn buckle. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Krishnan, RV and Venkataswamy, MA (1989) Report on Failed High Pressure Turbine Rotor Blades. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Venkataswamy, MA (1989) Report on the Examination of I Stage Compressor Blades. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Venkataswamy, MA (1989) Report on the Investigations on Failed Hydraulic Booster Jack. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Venkataswamy, MA (1989) Report on the examination of fracture of Cardon Shaft of R-11 engine and the examination of components from R-25 engine. Project Report. National Aerospace Laboratories, Bangalore.
Raghuram, AC and Rangaraju, R and Venkataswamy, MA and Krishnan, RV (1989) Examination of helicopter components. Project Report. National Aerospace Laboratories, Bangalore.
Raja, S and Pashilkar, AA and Sreedeep, R and Kamesh, JV (2006) Flutter control of a composite plate with piezoelectric multilayered actuators13;. Aerospace Science and Technology, 10 (5). pp. 435-441.
Raja, S and Rajappa, Shashikala and Janardhanam, S (2009) Aeroelastic testing of aerospace vehicles - Experiences gained during four decades. In: National Conference on Wind Tunnel Testing (2009-IT11), 12-14 Mar 2009, IISc., Bangalore.
Raja, S and Upadhya, AR (2007) Active control of wing flutter using piezoactuated surface. Journal of Aircraft, 44 (1). pp. 71-80. ISSN 0021-8669
Rajagopalan, E (1983) File copying from PDP-11 to UNIVAC-1100 using 8quot; Diskettes - A utility program. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajagopalan, N and Vasudevan, N and Gripps, W and Rajagopalan, SR and Ramaseshan, S (1978) New processes for black coatings useful in harnessing solar energy. I - A room temperature black chromium plating bath. In: Proceedings of the International Solar Energy Congress on Sun: Mankind's future source of energy, 16-21 Jan 1978, New Delhi, India.
Rajagopalan, S (1988) Base-exchange softener and cooling water system - Chemical treatment and method of (control) testing of water. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajamurthy, MS (1996) Generation of comprehensive longitudinal aerodynamic data using dynamic wind tunnel simulation. In: 34th Aerosoace sciences meeting and exhibit, 15-18 Jan 1996, Reno, NV.
Rajamurthy, MS (1997) Generation of comprehensive longitudinal aerodynamic data using dynamic wind-tunnel simulation. Journal of Aircraft, 34 (1). pp. 29-33. ISSN 0021-8669
Rajamurthy, MS (2002) Modelling of the nonlinear lift and pitching moment characteristics of 60-degree delta wing and wing-bodies. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, 5-8 Aug 2002, Monterey, California, United States.
Rajamurthy, MS (1995) A Novel Method of Estimating leutral Point Using Dynamic Wind Tunnel Simulation. Technical Report. National Aerospace Laboratories, Bangalore, India.
Rajamurthy, MS and Balakrishna, S (1990) Dynamic wind tunnel testing of a flexible wing model 13; 13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajamurthy, MS and Basappa, - (1995) Generation of Comprehensive Aerodynamic Data Using Dynamic Wind Tunnel Simulation. Technical Report. National Aerospace Laboratories, Bangalore, India.
Rajamurthy, MS and Subha, G and Basappa, MR (1993) Identification of the dynamics of a flexible delta wing model. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.
Rajan Kumar, - and Sundaramurthy, H and Prasada Rao, K (1997) Unsteady Pressure Measurements On 1 :40 Scale GSLV Heat Shield Model. Project Report. National Aerospace Laboratories, Bangalore.
Rajan Kumar, - and Viswanath, PR and Ramesh, ON (2003) Experimental investigation of side force control on circular cones using nose blunting. Project Report. National Aerospace Laboratories, Bangalore.
Rajani, BN and Govindaraju, L and Majumdar, Sekhar (2007) Numerical simulation of incompressible viscous flow past a pitching NACA0012 aerofoil. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Rajani, BN and Rohini, HS and Majumdar, Sekhar (2007) Numerical computation of turbulent flow in non-orthogonal duct junctions. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Rajappa, N and Leelavathi, K (1977) On smoothing airfoil section coordinate data. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajappa, N and Leelavathi, K (1980) A surface-fit approximation in aerodynamic calculations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajashekar, C and Shambhoo, - and Raghukumar, HS and Sriram, G and Kumar, SC and Athith, GUS and Vijayasankaran, K and Natarajan, R and Jeyaseelan, AR and Ashirvadam, K and Isaac, JJ (2021) Experimental studies on the thermoacoustics of afterburner screech combustion instabilities in a model afterburner test rig. In: Proceedings of the National Aerospace Propulsion Conference, Singapore.
Rajashekar, C and Shambhoo, R and Raghukumar, HS and Udaya Kumar, RM and Ashirvadam, K and Isaac, JJ (2021) High-Speed Shadowgraph Visualization Studies of the Effectiveness of Ventilating a V-Gutter Flame Holder to Mitigate Screech Combustion Instability in an Aero-Gas Turbine Afterburner. In: Design and Development of Aerospace Vehicles and Propulsion Systems, Singapore.
Rajeev, G and Jinde, P (2009) Design and development of a 2.5quot; diameter integral 6-component strain gage balance. In: National Conference on Wind Tunnel Testing 2009-CP15, 12-14 Mar 2009, IISc., Bangalore.
Rajeev , Kumar and Viswanath, PR (1997) The Influence of a Forward Splitter Plate on Base Pressure and Drag of Wedges. Technical Report. National Aerospace Laboratories, Bangalore,India.
Rajeeva, Kumar and Shyam, Chetty (1995) Flight CoptroI Design Using Multi -objective Multi -model optimisation Technique. Technical Report. National Aerospace Laboratories, Bangalore, India.
Rajeevalochanam, P and Nanjundaiah, VK and Sahadevan, SK and Sharma, Narndra and Janney, KS (2016) Comparative study of two and three blade mini propellers aerodynamic performance. In: Proceedings of the ASME Turbo Expo, 13-17 June 2016, Seoul, South Korea.
Rajendra, G (1994) 25 years of national trisonic aerodynamic facilities (NTAF). In: Aerodynamic Testing and Structural Dynamics. Interline Publishing Private Limited, Bangalore, pp. 1-18. ISBN 81-7296-040-9
Rajendra, G and Pandian, S and Shivaramakrishnan, AE and Varambally, BS (1987) Force measurements on RH-560 (APC-REX). Project Report. National Aerospace Laboratories, Bangalore.
Rajendra, G and Seshadri, SN and Jerath, VK (1971) Programs for evaluating body radius in accordance with transonic area rule. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajeswari, B and Dutt, HNV (1988) Analysis of wing flap configurations by a nonplanar vortex lattice method. Journal of Aircraft, 25 (2). pp. 97-98. ISSN 0021-8669
Rajeswari, B and Dutt, HNV (1985) Analysis of wings with leading edge and/or trailing edge segmented (spanwise) flaps using planar horse shoe vortex lattice method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajeswari, B and Dutt, HNV (1986) Nonplanar vortex lattice method for analysis of complex multiple lifting surfaces. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rajeswari, B and Prabhu, KR (1983) Estimation of flap schedule and minimum drag envelope. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Raju, Channa and Basu, Bharathibai J (2003) NAL Binary PSP: Aging Tests at Transonic Speeds- part III. Project Report. National Aerospace Laboratories, Bangalore.
Raju, Channa and Viswanath, PR (1998) Base Drag Reduction Caused by Riblets on a GAW(2) Airfoil. Journal of Aircraft, 35 (6). pp. 988-992.
Raju, Channa and Viswanath, PR and Jagadeeswarachar, SP (2003) PSP Measurements on an Aircraft Wing-Body and Slenderbody Models in the NAL1.2m Trisonic Wind Tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Ramabhadran, S and Sridharan, R (1982) Computation of the aerodynamic characteristics of wings in linearised supersonic flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramachandra, MS and Haque, CI and Narasimha Swamy, MR (1976) Design of contraction for the transonic cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramachandra, MS and Narasimha Swamy, MR (1985) Calibration of a 6 mm wedge probe for cascade wake measurements. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramakrishnan, SV and Subramanian, NR (1978) Flow past nonconical wings with separation. Journal of Aircraft, 15. pp. 383-384. ISSN 0021-8669
Ramamoorthy, P (1997) Derivation of four-digit airfoils from the Sunya airfoil. Journal of aircraft, 34 (3). pp. 441-443. ISSN 0021-8669
Ramamoorthy, P (1985) Role of computer aided design in the development of a new aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P (1988) A new method for designing natural laminar flow airfoils. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P and Dwarakanath, GS and Narayana, CL (1969) Wagner functions. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P and Narayana, CL (1969) A modified multhopp's lifting surface theory as programmed for the NAL sirius computer. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P and Narayana, CL and Dutta, Vimala (1977) Estimation of drag polar. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P and Sheela, BV (1973) Modification of the flexible polyhydron method for function minimisation. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P and Sinha, AK and Narayana, CL and Dutta, Vimala and Dwarakanath, GS and Sheela, BV (1976) Optimization of a passenger aircraft for minimum direct operating cost - A preliminary study. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamurthy, K and Shembharkar, TR and Pai, BR (1983) Prediction of film cooling with gaseous coolant injection. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamurthy, S and Murugesan, K (1991) Characterisation of Unsteady Flows in Centrifugal Impellers. In: 6th National Convention of Aerospace Engineers, 24 & 25 January 1991, IIT,Bombay. (Submitted)
Ramamurthy, S and Murugesan, K (1978) Test facility for turbo charger. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Ramamurthy, S and Murugesan, K and Prithviraj, D (1991) Flow behaviour in centrifugal impellers. In: 10th International Symposium on Air Breathing Engines, 1-6 Sep 1991, Nottingham, England.
Ramamurthy, S and Murugesan, K and Sankaranarayan, S (1986) Computer aided design of centrifugal impellers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamurthy, S and Murugesan, K and Sankaranarayanan, S (1987) Theoretical model for the performance evaluation of centrifugal compressors. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamurthy, TV and Mani, VSV (1978) Instrumentation system for helicopter rotor model. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Raman, KS (1994) Force Measurements on 1/35 Scale ASLV Model in 0.6m Transonic Wind Tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Ramarao, G (1964) Fusion welding of pressure vessels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramaswamy, MA (1974) Application of integral moment method to the hypersonic laminar near wake of a cold cylinder. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Ramaswamy, MA (1961) Design of transonic test-sections for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramaswamy, MA and Desikan, KS (1978) Annular sleeve type control valve with radial outflow for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramaswamy, MA and Kubota, Toshi (1972) Near wake of a cold circular cylinder AT M=6. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramaswamy, MA and Parikh, PC (1975) Pressure distribution of aerofoils if embedded supersonic region. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Ramaswamy, MA and Rajendra, G (1978) Experimental investigation of transonic flow past a blunt cone-cylinder. Journal of Spacecraft and Rockets, 15 (2). pp. 120-123. ISSN 0022-4650
Ramaswamy, MA and Sharma, Ramachandra and Krishnamurthy, K (1974) Two dimentional transonic blockage interference studies in the NAL 1-Ft. blowdown wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramaswamy, MA and Viswanathan, S (1975) Some observations on the Adams body of minimum wave drag. Journal of Aircraft, 12. pp. 1001-1002. ISSN 0021-8669
Ramaswamy, NA and Toshi kubota, -- (1972) Near wake of a cold circular cylinder. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Ramesh, G (1997) Development of an Interrogation System for Particle Imaging Velocimetry. Technical Report. National Aerospace Laboratories, Bangalore,India.
Ramesh, G and Madhavan, KT and Ahmed, Sajeer and Sudhakar, (2010) Development of synthetic Jet based flow control technique for Low Revnolds number applications. Project Report. NAL, Bangalore.
Ramesh, G and Sajeer, Ahmed (2009) Development of synthetic Jet Actuator for Active Flow control. Project Report. National Aerospace Laboratories, Bangalore.
Ramesh, G and Sajeer, Ahmed and Sudhakar, S (2008) Active flow control using synthetic Jet Actuator. Project Report. National Aerospace Laboratories, Bangalore.
Ramesh, G and Suriyanarayanan, P and Sudhakar, S Near Field Studies of an Elliptic Jet in a Co flow. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), 10-12 December 2009, Bangalore.
Ramesh, G and Verma, SB (2009) Investigation of near Field Flow of an Elliptic Jet in a Co-flowing Outer Stream using 2D PIV. Project Report. National Aerospace Laboratories, Bangalore.
Ramesh, MP (1990) Estimation of possible output from typical wind turbines in Talacauvery winds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, MP (1990) Short term comparative wind measurements on a part of Kappatagudda range during July 1990. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, MP and Shenoy, Kalpana S (1988) Wind speed data collected at NAL, B"lore during the interval January-June 1987. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, MP and Shenoy, Kalpana S (1988) Wind speed data collected at NAL, B'lore during the interval January-June 1988. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, MP and Shenoy, Kalpana S (1988) Wind speed data collected at NAL, B'lore during the interval July-December 1987. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, MP and Shenoy, Kalpana S (1988) Wind speed data collected in the Ridge Line around Talacauvery in Karnataka Westernghats during the Interval July-September 1988. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, MP and Shenoy, Kalpana S (1989) Wind speed data collected in the ridge line around Talacauvery in Karnataka Westernghats during the Interval January-March 1989. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramesh, NR and Natarajan, R (1991) Atomisation and combustion performance of a stem-jet type twin-fluid acoustic atomiser.13;. In: Proceedings of the 5th International Conference on Liquid Atomization and Spray Systems - ICLASS-91, 15-18 Jul 1991, Gaithersburg, MD, USA.
Ramesh, SV and Raol, JR and Shantha Kumar, N (1993) FIDA-Flight Data Analysis Package in PC-MATLAB. Technical Report. National Aerospace Laboratories, Bangalore, India.
Ramesh, TG and Shubha, V (2006) Thermal characterization of materials at high pressures. Journal of Materials Science, 41 (5). 1617-1 621. ISSN 0022-2461
Ramesh, V and Deshpande, SM (2007) Kinetic grid free method for flutter prediction in turbo-machines. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Ramesh, V and Deshpande, SM (2001) Least squares kinetic upwind method on moving grids for13; unsteady Ruler computations. Computers and Fluids, 30 (5). pp. 621-641.
Ramesh, V and Deshpande , SM Kinetic Meshfree method for flutter prediction in turbomachines. Sadhana Academy proceedings in Engineering Sciences. (Submitted)
Ramesh, V and Mathur, JS and Deshpande, SM (2007) Grid free euler computations using modified cir splitting. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Ramesh , G and Madhavan, KT and Sajeer, Ahmed (2009) Development of smart actuators for active flow control at low reynolds number. In: MAV Workshop Challenges and Preferred Outcomes, 13 November 2008, National Aerospace Laboratories.
Rangarajan, R and Ramaswamy, MR (1976) Design of 2nd DIA strain gauge balance with replaceable axial force unit. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rangarajan, R and Viswanathan, S (1970) Data reduction program for floating frame balances. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Ranjan, Vepa and Balasubramanian, TS (1979) Analytical studies on pitoe-flat stabidity of Helicopter rotors in hover and forward flight. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Rao, C.K. Narayana (1986) A feasibility study for a large low speed wind tunnel. Project Report. NAL, Bangalore.
Rao, C.K. Narayana (1986) Force Measurments on ASLV Boosterin the Vicinity of Core Vehicle. Project Report. NAL, Bangalore.
Rao, DM (1970) Hypersonic aerodynamic characteristics of flat delta and caret wing models at high incidence angles. Journal of Spacecraft and Rockets, 7 (12). pp. 1475-1476.
Rao, DM (1975) Hypersonic incipient separation on delta wing with trailing-edge flap. AIAA Journal, 13 (10). pp. 1386-1388. ISSN 0001-1452
Rao, DM (1975) Separated flow induced by trailing-edge flaps on delta wings at M = 8.2. Journal of Aeronautical Society of India, 27. pp. 17-21.
Rao, DM (1961) Some aspects of design of air storage system for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Rao, DM and Murthy, AV and Kashyap, RR (1976) A variable by-pass diffuser for supersonic wind tunnels. Journal of Aeronautical Society of India, 28. pp. 27-31.
Rao, DM and Nilakantan, P (1960) Note on compressed air capacity requirements for the 4-FT. Trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rao, DM and Rajendra, G and Sundaramurthy, H and Kanagarajan, V (1975) Contributions by NAL Aerodynamics Division at SLV-3 Review. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rao, DM and Raju, KN (1964) The use of splitters for flow control in wide angle conical diffusers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rao, DM and Seshadri, SN (1976) Application of Radial-Splitters for Improved wide-angle diffuser performance in blowdown tunnel. Journal of Aircraft, 13 (7). pp. 538-540. ISSN 0021-8669
Rao, Krishna KV and Sundararajan, D (1969) Whirl flutter of flapped blade rotor systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Rao, R Ramachandra and Roopa, HN and Kannan, TS (1993) Processing and characterisation of ceramic slurries Part I : Particle size distribution of ceramic particles in13; ceramic slurries. Technical Report. National Aerospace Laboratories, Bangalore, India.
Rao, R Ramachandra and Roopa, HN and Padmaja, RS and Kannan, TS (1993) Processing and characterisation of ceramic slurries . Part-IV : Study of sedimentation behaviour of ceramic slurries. Technical Report. National Aerospace Laboratories, Bangalore, India.
Rao, RMVGK and Rao, Sandhya and Sridhara, BK (2006) Studies on tensile and interlaminar shear strength properties of thermally cured and microwave cured glass-epoxy composites13;. Journal of Reinforced Plastics and Composites, 25 (7). pp. 783-795.
Raol, JR (1996) Feed forward neural networks for aerodynamic modelling and sensor failure detection. In: 47th Annual General Meeting of the Aeronautical Society of India, 6-8 Jan 1996, Madras, India.
Raol, JR (1993) Suggested Curriculum Activity on 'Identification13; Based Flight Test Experiments amp; Parameter Estimation Methodologies' for EFTS of ASTE. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Raol, JR and Balakrishna, S and Viswanatham, M (1980) Effect of pitch motion cue on human operator's performance in compensatory experiments. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Raol, JR and Girija, G (1998) Multisensor Data Strategies and Algorithms. Technical Report. National Aerospace Laboratories, Bangalore, India.
Raol, JR and Gopalratnam, G (1989) Estimation of aerodynamic derivatives of projectiles from aeroballistic range data using maximum likelihood method. In: Annual Paper Meeting 1989, 28 Jan 1989, Ranchi.
Raol, JR and Jategaonkar, RV (1995) Artificial Neural Network for Aerodynamic Modeling. Technical Report. National Aerospace Laboratories, Bangalore, India.
Raol, JR and Parameswaran, V (1993) Recursive estimation of model error for identification of nonlinear continuous time systems. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.
Raol, JR and Ramesh, SV and Kavitha, B (1993) Parameter estimation of state space models by hopfield neural network. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Raol, JR and Saraswathi, L and Girija, G (1993) Helicopter Flight Test Specifications for Parameter Estimation. Technical Report. National Aerospace Laboratories, Bangalore, India.
Ravichandran, KS (1993) Difference schemes for hyperbolic system of Conservation Laws 13; 13;. In: CFD: Advances and Applications, 1993, Bangalore, India.
Ravichandran, KS (1993) Introduction to multigrid methods. In: CFD: Advances and Applications, 1993, India.
Ravichandran, KS and Rangarajan, R and Desai, SS and George, KP (1988) Vortex simulation in full potential solver on a cartesian grid. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Ravishankar, S and Dutt, HNV and Gurumoorthy, B (2010) Automated inspection of aircraft parts using a modified ICP algorithm , H. N. V. Dutt and B. International Journal of Manufacturing Technology, 46 (1-4). pp. 227-236.
Reddy, KS and Lokesha, H and Akhila, S (2015) Video stabilization for micro air vehicles. International Journal of Advanced Research in Computer and Communication Engineering , 4 (4). pp. 442-445. ISSN 2278-1021
Renukadevi, M and Girija, G and Ganesan, S and Subbaraya, BL (1980) Programmable voltage and current waveform generator. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Renukadevi, M and Girija, G and Subbaraya, BL and Ganesan, S (1980) Progrmmable voltage and current waveform generator. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sahoo, S and Priyadarshini, L and Shekhar, G (2015) Flight Test Instrumentation System for a Typical Prototype Civil Aircraft. International Journal of Control Theory and Applications, 8 (3). pp. 977-983.
Sajeer, Ahmed and Mathur, NB and Manisankar, C (2008) Evaluation of Aerodynamic Performance of Sidewall Compression Intake Relevant to Airbreathing Propulsion Vehicles for Intake Flow Entry at M=4.0. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sajeer, Ahmed and Selvarajan, S (1985) Pressure measurements in the heat shield region of 1/80 scale PSLV model In the mach number range of 0.8 to 4.0. Project Report. National Aerospace Laboratories, Bangalore.
Sajeer, Ahmed and Selvarajan, S and Varambally, BS and Sivaramakrishnan, AE and Pandyan, S (1987) Steady pressure measurements in the strap on booster interference Region of 1/20 scale ASLV configuration. Project Report. National Aerospace Laboratories, Bangalore.
Sajeer, Ahmed and Sudhakar, S (2010) Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations. Project Report. National Aerospace Laboratories, Bangalore.
Sajeer, Ahmed and Suriyanarayanan, P and Madhavan, KT and Ramesh, G Studies on Eppler 61 Airfoil with Gurney Flaps at Low Reynolds numbers. Project Report. NAL.
Sajjan, Sharanappa V and Sengupta, TK (2007) Interaction between a spanwise convecting vortex and an airfoil. In: 4th International Conference on Theoretical, Applied, Computational and Experimental Mechanics (ICTACEM), 27-29 Dec 2007, Kharagpur, India.
Sajjan, Sharanappa V and Sengupta, TK (2007) Unsteady airfoil aerodynamics and dynamic stall. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Sangeetha, C and Rajani, BN and Majumdar, Sekhar (2000) Numerical Computation of Laminar FLOW Around a Square Cylinder. Project Report. National Aerospace Laboratories, Bangalore, India.
Sankar, N and Govindarajaswamy, E and Perumal, A and Muthuvel, S (2001) Dwell Control for RF Sputtering. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sankar, N and Govindarajaswamy, E and Perumal, A and Muthuvel, S (2001) PC based braider control. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sankar, R and Panchapakesan, S (1970) Solution of very large systems of equations arising out of biharmonic equations, using iterative methods. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sankaranarayanan, S and Paranjpe, PA (1978) Application of turbopack in solar energy systems. In: Proceedings of the International Solar Energy Congress on Sun: Mankind's future source of energy, 16-21 Jan 1978, New Delhi, India.
Sankaranarayanan, S and Ramamurthy, S and Murugesan, K and Ramachar, D (1986) Establishment of closed circuit centrifugal compressor test rig (CLOCTER). Technical Report. National Aeronautical Laboratory, Bangalore,India.
Sankaranarayanan, S and Roshan, Antony and Suraj, CS Technology Driven Programme for the Development for the Development of a Fixed wing micro Air Vehicle at NALDRIVEN. In: MAV Workshop- Challenges and Presferred Outcomes, 13 November 2008, National Aerospace Laboratories.
Santharam, A (1991) "Split control surface modelling for reconfiguration". Project Report. National Aerospace Laboratories, Bangalore.
Sapre, AV (1990) On use of remotely sensed land surface data from satellite for preliminary wind resource assessment. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sarasamma, VR (1976) Smoothening of airfoil coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sathia Narayanan, A and Ahmed, Sajeer and Viji, M (2009) Empirical Evaluation of Wall Interference Effects on a Laminar Supercritical Airfoil at Transonic Speeds. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, Bangalore.
Sathia Narayanan, A and Verma, SB (2015) Experimental investigation of a Mach 4 shock-wave turbulent boundary layer interaction near an expansion corner. In: 53rd AIAA Aerospace Sciences Meeting, 5-9 January 2015, Kissimmee, Florida.
Satish Kumar, S and Kumar, L and Senthil Kumaran, R and Kumar, VS and Shobhavathy, MT (2019) Design of high transonic axial compressor stage for small gas turbine applications. In: ASME 2019 Gas Turbine India Conference, GTINDIA 2019, December 5–6, 2019, Chennai, Tamil Nadu, India.
Satyanarayana, B and Irani, PA (1961) Aerodynamic design of two dimensional supersonic nozzle contours with boundary layer corrections. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Savanur, RA and Mudkavi, Vidyadhar Y (2009) Structural and Aerodynamic analysis of AGARD 445.6 Wing ANSYS using Panel Method. Technical Report. NAL.
Savanur, RA and Sharanappa, Sajjan V and Mudkavi, Vidyadhar Y (2009) Two dimensional analysis of aerofoil sections for 500 kW horizontal-axis wind turbine. Technical Report. NAL.
Saxena, SK and Nair, Manoj T (2004) Development and Critical Assessment of Technology for Numerical Simulation of Hypersonic Real Gas Flows. Project Report. National Aerospace Laboratories, Bangalore, India.
Saxena, SK and Ravi, K (1995) Computation of three dimensional supersonic and hypersonic blunt body flows using high resolution TVD schemes based on Roe's Approximate Riemann Solver. Lecture Notes in Physics (453). pp. 520-524.
Saxena, SK and Ravi, K (1995) Computation of three dimensional supersonic and hypersonic blunt body flows using high resolution TVD schemes based on Roe's approximate Riemann Solver. In: 14th International Conference on Numerical Methods in Fluid Dynamics, 11-15 July 1994, Bangalore, India.
Saxena, SK and Ravi, K (1994) Ground tests to minimize development risks and limit the number of development cycles. In: 12th AIAA Applied Aerodynamics Conference, 20-22 June 1994, Colorado Springs.
Saxena, SK and Ravi, K (1995) Some aspects of high-speed blunt body flow computations with Roe scheme. AIAA Journal, 33 (6). pp. 1025-1031.
Seetharam, HC and Rangarajan, R (1970) Force calibration of AGARD B model in transonic flow mach numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sekar, Y and Pankaj, AC and Manjuprasad, M (2016) Reliability studies on the influence of joint clearance on the kinematics of the nose landing gear mechanism of a transport aircraft using contact theory. ARPN Journal of Engineering and Applied Sciences, 11 (18). pp. 11049-11055. ISSN 18196608
Selvakumar, N and Pradhan, U and Krupanidhi, SB and Barshilia, Harish C (2016) Structural and optical properties of graphene oxide prepared by modified hummers' method. Computers, Materials and Continua, 52 (3). pp. 173-184. ISSN 15462218
Selvarajan, S Wind tunnel force measurements on 1/40 scale PSLV strap-on boosters. Project Report. National Aerospace Laboratories, Bangalore.
Selvarajan, S and Arokkiaswamy, A and Kanagarajan, V (1988) Wind Tunnel Force Measurements on 1/12 Scale Model of PRITHVI missile Configuration - II : Final Report. Project Report. National Aerospace Laboratories, Bangalore.
Selvarajan, S and Ram, Vasanta V (1994) Dynamical characteristics of wave-excited channel flow. Sadhana, 19 (Part 3). pp. 349-360. ISSN 0256-2499
Sengupta, TK and Kasliwala, A and De, S and Nair, Manoj T (2003) Temporal flow instability for Magnus - Robins effect at high rotation rates. Journal of Fluids and Structures, 17 (7). pp. 941-953.
Sengupta, TK and Selvarajan, S (1988) Study of flow past a circular cylinder using a higher order scheme for navier-stokes equation. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Senthil Kumaran, R and Swamy, KMM (2006) CASCADE TESTS ON CE 20 LOX TURBINE SECOND ROTOR BLADE PROFILE. Technical Report. National Aerospace Laboratories, Bangalore.
Senthil Kumaran, R and Swamy, KMM (2006) CASCADE TESTS ON CE 20 LOX TURBINE STATOR BLADE PROFILE. Technical Report. National Aerospace Laboratories, Bangalore.
Seshadri, SN (1985) Aerodynamic data base generation for combat aircraft configurations - A project proposal. Technical Report. National Aerospace Laboratories, Bangalore.
Seshadri, SN and Narayan, KY (1986) Lee Surface Flovv Over Delta Wings at Supersonic Speeds - Some Features of Different Types of Flow. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Seshadri, SN and Narayan, KY (1988) Possible types of flow on lee-surface of delta wings at supersonic speeds. Aeronautical Journal, 92. pp. 185-199. ISSN 0001-9240
Seshadri, SN and Rajendra, G (1974) Appplication of the method of axial source for calculation of subcritical pressure distribution on 'Not'slender axisymmetric bodies at zero lift. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Seshadri, SN and Rao, DM (1974) On the application of radial-splitters flow spreaders in the NAL 1-FT. blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Shanbhag, VV and Rao, RU (1970) Formal force characteristics of cone-cylinder and ogive cylinder bodies at mach number = 1.8. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Shankar, PN (1976) Effects of geometry and reynolds number on savonious type rotors. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Shankar, PN (1991) Exact Solutions for a Class of Nonlinear Free Surface Flows. Technical Report. National Aerospace Laboratories, Bangalore, India.
Shankar, PN (1975) On the aerodynamics performance of a class vertical axis windmills. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Shankar, PN (1992) On the shape of a two-dimensional bubble in uniform motion. Journal of Fluid Mechanics, 244. pp. 187-200.
Shankar, PN (1984) A note on a class of exact solutions in invisced rotational flows. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Shankar, PN and Kidambi, R (2009) Mixing in internally stirred flows. Proceedings of the Royal Society of London, Series A (Mathematical, Physical and Engineering Sciences), 465. pp. 1271-1290. ISSN 1364-5021
Shankar, PN and Kumar, M (1994) Toroidal vortex rings. Current Science, 66 (2). pp. 151-153.
Shankar, PN and Narasimhaiah, - (1977) Preliminary aerodynamic design data sheets for horizontal axis wind mills. Technical Report. National Aerospace Laboratories, Bangalore, India.
Shankar, Vijaya CS and Murthy, Srinivasa R and Singh, Prem M (1985) General specifications for a captive power driven compressors and dryer system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Shanmugam, P and Raja, S and Parammasivam, KM (2016) A study on VGTM actuation system for multi-axis morphing wing of UAV. In: 34th AIAA Applied Aerodynamics Conference, 13-17 June 2016, Washington, D.C..
Shantha Kumar, N (1995) Sensor Failure Detection and Management Scheme for Pressure Probes Kalman Filtering Technique. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sharanappa, Sajjan V and Padmanabhan, MA and Mandal, S and SenGupta, G and Dutta, PK (2011) Unsteady RANS based impulse response studies of AGARD wing for aeroelastic and flutter analysis. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Sharanappa, Sajjan V and Siva Kumar , K (2013) Effect of Aerofoil Thickness and Camber on the Flapping Aerofoil Propulsion. In: The 2nd International Conference on Recent Advances in Design, Development and Operation of Micro Air Vehicles - 2013, 21 - 23 November, 2013, Jawaharlal Nehru Technological University Hyderabad (JNTUH), India.
Sharanappa, Sajjan V and Siva Kumar , K (2013) Effect of Various Parameters on the Flapping Motion of an Aerofoil. Frontiers in aerospace Engineering, 2 (2). pp. 129-135. ISSN 2325-6796
Sharanappa, Sajjan V and Siva Kumar , K (2012) Reynolds-Averaged Navier-Stokes Computations over a Two-element Aerofoil. International Journal of Systems , Algorithms & Applications , 2 (Specia). pp. 38-42. ISSN ISSN Online: 2277-2677
Sharath, PP and Senthil Kumaran, R and Jagannatha Rao, B and Poornima, N (2009) CALIBRATION OF PITOT STATIC PROBES FOR HAL, KORAPUT. Technical Report. National Aerospace Laboratories, Bangalore.
Sharma, RC and Gopinath, N and Karthik, N (2009) Concept study of fin mounted tail plane for pitch-up alleviation of LCA. Technical Report. National Aerospace Laboratories, Bangalore, India.
Shashikanth, BN and Kidambi, R (2021) The Centroid-Deformation Decomposition for Buoyant Vortex Patch Motion. Regular and Chaotic Dynamics, 26 (6). pp. 577-599.
Sheela, BV and Ramamoorthy, P (1973) Swift A New constrained optimization technique. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Shembharkar, TR and Pai, BR (1982) Predictions of heat transfer in turbine blades with a 2-equation model of turbulence. In: Heat transfer 1982; Proceedings of the Seventh International, 6-10 Sept 1982, Munich, West Germany.
Shibu, PS and Sandeep, - and Choudhury, Balamati and Nair, RU (2021) Multi-objective Optimization Approach for Low RCS Aerodynamic Design of Aerospace Structures. In: Design and Development of Aerospace Vehicles and Propulsion Systems, Singapore.
Shivakumar Swamy, M (1985) Parametric Studies of Aft-Body Drag. Project Report. National Aerospace Laboratories, Bangalore.
Shivakumar Swamy, M (1985) Specification for tubestack of inter cylinder cooler. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Shivakumar Swamy, M (1994) Store separation simulation studies in high speed wind tunnels. In: Aerodynamic Testing and Structural Dynamics. Interline Publishing Private Limited, Bangalore, pp. 1-18.
Shivakumara, C Sample1. Sample1.
Shobhavathy, MT (2011) CFD analysis to investigate the effect of axial spacing in a single stage transonic axial flow compressor. In: International Symposium on Applied Aerodynamics and Design of Aerospace Vehicle , 16-18 Nov 2011, Bangalore, India.
Shruti, K and Sivapragasam, M (2021) Numerical Investigation on the Effect of Propeller Slipstream on the Performance of Wing at Low Reynolds Numbers. In: Design and Development of Aerospace Vehicles and Propulsion Systems, Singapore.
Shubha, G (1995) MIS -Menu Initialisation Software. Technical Report. National Aerospace Laboratories, Bangalore, India.
Shubha, V and Ramesh, TG (1986) Temperature programmer for the teflon-cell arrangement in high pressure studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, AK (1993) Analysis of C60 Fullerite Compression Under Non-Hydrostatic Pressure. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, AK (1993) The Lattice Strains in a Specimen (Cubic System) Compressed Non Hydrostatically in an opposed Anvil Device. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, AK and Menendez, PE and Gutierrez, G and Akahama, Y and Kawamura, H (2006) Nonhydrostatic compression of bismuth to 222GPa: Some constraints on elasticity of the bcc-phase13;. Journal of the Physics and Chemistry of Solids, 67 (9-10). pp. 2192-2196.
Singh, DB and Suprabha, PS and Gopinath, PR and Muralidhara, HS and Mohan, SR and Koner, D (2011) Calibration of conical mass flow control device for air intake model tests. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Singh, DB and Suryanarayana, GK (2016) Application of Fiber Bragg Grating Sensors for Dynamic Tests in Wind Tunnels. Journal of the Indian Institute of Science, 96 (1 (Jan). pp. 47-52. ISSN 0970-4140
Singh, JP (1999) Accelerated and robust finite volume Navier-Stokes solver for all speeds. Sadhana - Academy Proceedings in Engineering Sciences, 24 (1-2). pp. 121-145. ISSN 0256-2499
Singh, JP (1983) Computation of viscus transonic flow over airfoils comparisons and compilation of results. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, JP (1996) Computational Aeroacoustics of propeller driven aircraft:A status report. Technical Report. National Aerospace Laboratories, Bangalore,India.
Singh, JP (1995) Evaluation of Jameson-Schmidt-Turkel dissipation scheme for hypersonic flow computations. In: 13th AIAA Applied Aerodynamics Conference, 19-22 June 1995, San Diego, CA.
Singh, JP (1996) Evaluation of Jameson-Schmidt-Turkel dissipation scheme for hypersonic flow computations. Journal of Aircraft, 33 (2). pp. 286-290. ISSN 0021-8669
Singh, JP (1998) Some Thoughts Towards Long-Term Ramp;D Activities in Aero-and Vibro- Acoustics at NAL. Technical Report. National Aerospace Laboratories, Bangalore, india.
Singh, JP and Rangarajan, R and Desai, SS (1988) On the assessment of quot;Correctabilityquot; of data in two-dimensional transonic wind tunnel tests. Technical Report. National Aeronautical Laboratory, Bangalor, India.
Singh, JP and Rangarajan, R and Ramaswamy, MA (1985) Computatian of flow over airfoils under high 11ft separated flow conditions. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, JP and Rangarajan, R and Ramaswamy, MA (1988) Computation of flow over airfoils under high lift separated flow condition 13; 13;. Journal of Aeronautical Society of India, 40. pp. 105-110.
Singh, JP and Viswanathan, S and Rangarajan, R and Desai, SS (1996) Notes on the adaptation and validation of a panel code NALSOF0509 for the calculation of pressure distribution and overall coefficients on wings, bodies and wing-body-tail combinations in sub- and supersonic flows. Project Report. NAL, Bangalore.
Singh, KP and Mathur, JS and Ashok, V and Chakraborty, Debasis (2010) Computational fluid dynamics in aerospace industry in India. Defence Science Journal, 60 (6). pp. 639-652. ISSN 0011-748X
Singh, Karan and Murugesan, K (1974) Design of a highly loaded gas turbine stage. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, Manish K (2011) Modified CIR Scheme for Mesh-free Euler Solver. In: Meshfree-2011 Conference, 10-11 January 2011, Aerospace Department, Indian Institute of Science, Bangalore.
Singh, Manish K and Dhanalakshmi, K and Chakrabartty, SK (2006) Navier-Stokes Analysis of Airfoils with Gurney Flap. Project Report. National Aerospace Laboratories, Bangalore.
Singh, Manish K and Dhanalakshmi, K and Mathur, JS (2011) Characterization of RTA 21463 Wing and Estimation of Drag divergence Mach number. Project Report. CSIR-NAL, Bangalore.
Singh, Manish K and Dhanalakshmi, K and Mathur, JS (2009) Computation of Two Dimensional Flow past Multi Element Airfoils. Project Report. National Aerospace Laboratories, Bangalore.
Singh, Manish K and Dhanalakshmi, K and Mathur, JS (2009) Effect of Gap on the Aerodynamic Performance of RTA 7025 Double Slotted Airfoil. Project Report. National Aerospace Laboratories, Bangalore.
Singh, Manish K and Dhanalakshmi, K and Mathur, JS (2012) Estimation of Drag divergence Mach number for General Transport wing. In: 14th AeSI CFD Symposium, 10-11 August 2012, Aerospace Engineering Department, I.I.Sc. Bangalore.
Singh, Manish K and Dhanalakshmi, K and Meenakshi, and Mathur, JS (2011) Drag divergence Mach number for NCAD-21463 Wing with 20 leading edge sweep angle. Project Report. CSIR-NAL, Bangalore.
Singh, Manish K and Madhu Babu, K and Dhanalakshmi, K and Mathur, JS (2012) Euler Simulation of NCA-F90-D-OV-112 Aircraft Configuration. Project Report. CSIR-NAL, Bangalore.
Singh, Manish K and Ramesh, V and Balakrishnan, N (2010) Convergence Acceleration of Mesh-less Euler Solver. In: 12th annual AeSI CFD Symposium, 11-12 August , Indian Institute of Science, Bangalore. (Submitted)
Singh, Manish K and Ramesh, V and Balakrishnan, N (2012) An implicit scheme for a meshless Euler solver. In: 26th National Convetion of Aerospace Engineers:Expanding frontiers in aerospace technologies-challenges and opportunities, 24-25 November 2012, Hyderabad.
Singh, Manish K and Ramesh, V and Deshpande, SM (2009) Mesh less Euler Computation for Cropped Delta Wing with Aileron Deflection. In: 11th Annual CFD Symposium, 11-12th August, Inidian Institute of Science, Bangalore.
Singh, Manish K and Ramesh, V and Mathur, JS and Deshpande, SM (2008) Application of Modified CIR Splitting with Grid-Free Method. Technical Report. National Aerospace Laboratories, Bangalore.
Singh, DB and Shawani, AL (2021) Enhancement in wind tunnel data acquisition system using NI-LabVIEW. In: AIP Conference Proceedings.
Sinha, UN (1993) Computation of inviscid flows: Various approximations. In: CFD: Advances and Applications, 1993, Bangalore, India.
Sinha, UN and Gissler, R and Sunder, R (1990) Transonic small perturbation code on suprenum. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN and Ramaswamy, MA (1974) Preliminary results of the computation of pressure distribution on a super critical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN and Ramaswamy, MA (1974) Priliminary results of the computation of pressure distribution on a supercritical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN and Sarasamma, VR (1988) An iterative scheme for numerical solution of transonic small perturbation equation. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN and Sarasamma, VR and Rajalakshmy, S and Sreenivasan, CR and Dwarakanath, GS (1993) Development of parallel processing at NAL: A retrospect 13; 13;. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 1993, Sikkim, India.
Sinha, UN and Sarasamma, VR and Sreenivasan, CR and Sivaramakrishnan, Rajalakshmy and Shridhar, N (1988) Sequential and parallelised version of transonic small perturbation code on flosolver. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN and Singh, JP (1979) Computation of axisymmetric inviscid transonic flow past ellipsoids of revolution. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Siva Kumar, K and Sharanappa, Sajjan V (2011) Unsteady Flow past a Combined Pitching and Plunging Aerofoil using an Implicit RANS Solver. In: International Conference on Mechanical and Aerospace Engineering (CMAE 2011), 21-23 Mar 2011, New Delhi, India.
Siva Kumar, K and Sharanappa, Sajjan V (2012) Unsteady Flow past a Flapping Aerofoil. TRANSACTION ON CONTROL AND MECHANICAL SYSTEMS, 1 (1). pp. 43-48.
Siva Kumar , K and Sajjan, Sharanappa V (2013) Three-dimensional Unsteady Flow over a Heaving Rectangular Wing. Frontiers in Aerospace Engineering, Volume (Issue ). pp. 199-206. ISSN 2325-6796
Siva Kumar , K and Sharanappa, Sajjan V (2010) Computation of Unsteady Flow over a Plunging Aerofoil Using an Implicit Reynolds Averaged Navier-Stokes Solver. In: The 8th Asian Computational Fluid Dynamics Conference, 10-01-2010 to 14-01-2010, Hong Kong.
Siva Kumar , K and Sharanappa, Sajjan V (2012) Numerical Computation of Unsteady Compressible Flow past a Plunging Aerofoil. Journal of Applied Fluid Mechanics, 5 (4). pp. 131-138. ISSN 1735-3572
Siva Kumar , K and Sharanappa, Sajjan V Numerical Simulation of Unsteady Flow over the Heaving bodies. Technical Report. NAL.
Siva Kumar , K and Sharanappa, Sajjan V RANS Computation of Unsteady Flow past a Combined Pitching and Plunging Aerofoil. Documentation. NAL.
Siva Kumar , K and Sharanappa, Sajjan V (2011) Unsteady Compressible Flow over Heaving Bodies Using an Implicit RANS Solver. Applied Mechanics and Materials, Vols. . pp. 4589-4597. ISSN ISSN: 1662-7482
Siva Kumar , K and Sharanappa, Sajjan V (2011) Unsteady Flow past a Combined Pitching and Plunging Aerofoil using an Implicit RANS Solver. In: 2011 International Conference on Mechanical and Aerospace Engineering (CMAE 2011), March 21-23, 2011, SRM University, Modi Nagar Campus, Delhi-Meerut Road, Sikrikalan Modi Nagar, Gazhiabad, Uttar Pradesh - 201 204.
Siva Kumar , K and Sharanappa, Sajjan V (2011) Unsteady Flow past a Combined Pitching and Plunging Aerofoil using an Implicit RANS Solver. Applied Mechanics and Materials, Vols. . pp. 3481-3488. ISSN 1662-7482
Siva Kumar , K and Sharanappa , Sajjan V Numerical Simulation of Unsteady Flow over a Plunging Aerofoil Using an Implicit Reynolds Averaged Navier-Stokes Solver. Documentation. NAL, NAL.
Sivam, - and Verma, SB (2019) Study of vortex breakdown and pitch up on a compound delta wing. INCAS Bulletin, 11 (2). pp. 171-178. ISSN 20668201
Sivasankaram, K and Abbey, DK (1978) Note on orifice flow metering for compressible fluids. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Somashekar, BR (1974) Application of digital computers in vibration testing and analysis. In: Seminar on the Role of Computers in Structural Analysis, Design and Optimisation, 13-14 June 1974, Bangalore, India.
Somashekar, BR (1971) The effect of aerodynamic lag on the bending response of wings at supersong speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sreenath, P and Shambhoo,, - and Rajashekar, C and Davis, A and Isaac, JJ and Raghukumar, HS (2021) Triggering of flow instabilities by simulated sub/supercritical rayleigh heat addition in an aero-gas turbine afterburner. In: Proceedings of the National Aerospace Propulsion Conference, Singapore.
Sreenivasan, NR (1974) Analysis of the strength of turbine wheels and hubs. In: Seminar on the Role of Computers in Structural Analysis, Design and Optimisation, 13-14 June 1974, Bangalore.
Sreenivasan, Sheila and Srikantan, KV (1988) Additional channel data acquisition through analogue tape recorder. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sridharan, R (1986) A computer code for generating plots of aerodynamic data13; from wind tunnel tests. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sridharan, R and Viswanathan, S (1985) A Computer Code for Generating Plots of Load Distribution on Spanwise Sections on a wing. Project Report. National Aerospace Laboratories, Bangalore.
Srikantan, KV (1988) Additional standard wind tunnel balances for NTAF complex. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srikantan, KV (1975) Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srikantan, KV and Joseph, KA (1985) Gauging details of drag balance for use in Low speed wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.
Srikantan, KV and Joseph, KA (1985) Gauging details of drag balance for use in low speed wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srikantan, KV and Mahalingam, V (1975) Blowdown sequence-sequential logic display for the N.A.L.4'*4' trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srikantan, KV and Nirmala, GV (1988) Instrumentation for unsteady pressure measurement on cone cylinder configuration in NAL 1.2m Trisonic Wind 13; Tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srikanth, K and Rajeev, Kumar (2003) Improved Flow Visualization Studies in Water and Low-Speed Wind Tunnels. Project Report. National Aerospace Laboratories, Bangalore.
Srilatha, KR and Narayana, CL and Mudkavi, Vidyadhar Y and Premalatha, (2007) Aerodynamic analysis of a low aspect ratio wing-body-fin shuttle-like configuration in various flight conditions using panel method. In: 7th Asian Computational Fluid Dynamics Conference (ACFD7), 26-30 Nov 2007, Bangalore, India.
Srinathkumar, S (2005) Design of helicopter stability augmentation system using eigenstructure assignment and minimal order functional observers13;. Annual Forum Proceedings - AHS International, 2 (6). pp. 1170-1182.
Srinathkumar, S and Doherr, KF (1993) DLR-NAL Collaboration in the area of flight mechanics:Status Report 1983-1993. Technical Report. National Aerospace Laboratories, Bangalore, India.
Srinivas, CK and Sunithamma, J and Jha, RM (2004) High-frequency radiation pattern of slot antenna on a general paraboloid of revolution13;. IEEE Antennas and Propagation Society, 2. pp. 2023-2026.
Srinivas, J and Prateesh Kumar, P and Sathiyamoorthy, K and Venu, G (2013) Development of automated test sequence for mach 3.5 propulsion test facility. In: International Symposium on Air Breathing Engines (ISABE-2013-1306), 9-13 Sep. 2013, Busan, Korea.
Srinivas, K (1980) Computation of changes in the far flow field due to changes in the nose geometry of a typical fuselage. Technical Report. National Aerospace Laboratory, Bangalore, India.
Srinivas, K and Seetharam, SA and Murthy, Venkatesha A (1980) Experimental studies On-Ludwieg tube flows-I. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srinivasa, C (1995) Multigrid Technique Applied for the Full Potential Equation Over An Airfoil. Technical Report. National Aerospace Laboratories, Bangalore, India.
Srinivasa, K (1980) Computation of unsteady, one-dimensional flow with a shock-wave-shock fitting approach. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srinivasan, NR (1971) Analysis and design of high speed compressor and turbine rotors. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srinivasan, Santhakumari and Klika, Michael and Ludwig, Martin Heiko and Ram, Vasanta V (1994) A beginner's guide to the use of the spectral collocation method for solving some eigenvalue problems in fluid mechanics. Technical Report. National Aerospace Laboratories, Bangalore, India.
Srinivasan, V (1973) A united theory for the portevin-Le chateler effect in substitutional alloys. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Srivastava, A and Sharma, N and Srinivasa, C (1991) Aerodynamic analysis of NAL Light Aircraft Wing using a vortex lattice program. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srivastava, Ashok (1993) Panel methods. In: CFD: Advances and Applications, 1993, India.
Srivastava, Ashok (1991) Quadrilateral vortex panel code - Theory document. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srivastava, Ashok and Mook, Dean T (1995) An Improved Vortex Method for Closed Surfaces. Technical Report. National Aerospace Laboratories, Bangalore, India.
Srivastava, Ashok and Mook, Dean T (1994) Redundancy in the discrete-vortex method for closed bodies. Journal of Aircraft, 31 (6). pp. 1436-1437. ISSN 0021-8669
Srivastava, Meenu and William Grips, VK and Rajam, KS (2005) Electrodeposition of Ni-Co alloys from sulphamate bath. In: 59th Annual Technical Meeting of the Indian Institute of Metals, 15-16 Nov 2005, Chennai, India.
Srivastava, Meenu and William Grips, VK and Rajam, KS (2005) Electrodeposition of Ni-Co alloys from sulphate bath. -, 58 (5). ISSN 0972-2815
Subaschandar, N (1996) Development of a Boundary Layer Code Using K-C Model of Turbulence. Technical Report. National Aerospace Laboratories, Bangalore, India.
Subaschandar, N and Prabhu, A (1999) Turbulent near-wake development behind a flat plate13;. Aerospace Science and Technology, 3 (2). pp. 61-70. ISSN 1270-9638
Subaschandar, N and Prabhu, A (1999) Turbulent near-wake development behind a flat plate13; 13;. Aerospace Science and Technology, 3 (2). pp. 61-70. ISSN 1270-9638
Subaschandar, N and Prabhu, A (2002) Turbulent near-wake studies behind an infinitely swept wing. Journal of Aircraft, 39 (2). pp. 290-295. ISSN 0021-8669
Subaschandar, N and Rajeev, Kumar and Sundaram, S (1995) Drag Reduction Due to Riblets on a NACA 0012 Airfoil at Higher Angles of attack. Technical Report. National Aerospace Laboratories, Bangalore, India.
Subaschandar, N and Rajeev , Kumar and Sundaram, S (1999) Drag Reduction Due to Riblets on a GAW(2) Airfoil. Journal of Aircraft, 36 (5). pp. 890-892.
Subaschandar, N and Rajeev , Kumar and Sundaram, S (1995) Drag reduction due to riblets on a NACA 0012 airfoil at higher angles of attack. Technical Report. National Aerospace Laboratories, Bangalore.
Subrahmanyam, S and Murthy, GK and Paranjpe, PA (1974) Pyrogenic ignition system for afterburners. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Subramanian, NR and Chakrabartty, SK (1984) Computation of inviscid transonic flow past aerofoils using body fitted coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Subramanian, NR and Ramakrishnan, SV (1977) Dynamic stability derivatives of missile configurations (Theoretical evaluation). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Subramanian, NR and Siddalingappa, SR (1986) Computations with 3-D Euler code for wings. In: 2nd National Conference on Aerodynamics, 19-20 Dec 1986, Bangalore, India.
Subramanian, NR and Siddalingappa, SR (1986) Computations with 3-D Euler code for wings. Journal of Aeronautical Society of India, 38. pp. 241-248.
Sudhakar, S and Chandan Kumar, A and Arivoli, D and Dodamani, Ravi and Venkatakrishnan, L (2013) Experimental studies of propeller induced flow over typical micro air vehicle - AIAA 2013-0060. In: 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition , 07-10 Jan 2013, Grapevine (Dallas/Ft. Worth Region), Texas.
Sudhakar, S and Karthikeyan, N (2013) Effect of Leading edge tubercles on flow field over NACA-4415 airfoil at low Reynolds number. In: The 14th Asian Congress of Fluid Mechanics , 15 Oct 2013, Hanoi and Halong, Vietnam.
Sudhakar, S and Suriyanarayanan, P and Ramesh, G 2D-PIV Measurement in an elliptic Jet with Co-flow. In: 13th Asian Congress of Fluid Mechanics (ACFM), 17-21 December 2010, Dhaka, Bangladesh.
Sudhakar, S and Karthikeyan, N (2021) Flow Separation Control on a NACA-4415 Airfoil at Low Reynolds Number. In: Proceedings of 16th Asian Congress of Fluid Mechanics, Singapore.
Sudhakar, S and Karthikeyan, N and Suriyanarayanan, P (2019) Experimental studies on the effect of leading-edge tubercles on laminar separation bubble. In: 52nd Aerospace Sciences Meeting, 13–17 January 2014, National Harbor, MD.
Sujata, M and Madan, M and Raghavendra, K and Jagannathan, N and Bhaumik, SK Unraveling the cause of an aircraft accident. Engineering Failure Analysis, 97. pp. 740-758. ISSN 13506307
Sundaram, S (1989) Calibration of vane anemometer. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaram, S (2001) Investigation of Hysteresis Effects on a Swept Wing/Flap Configuration at High-Lift. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sundaram, S (2000) Survey of Experimental Investigations on Lift Enhancement Using Gurney Flaps. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sundaram, S and Vishwanath, PR and Subhaschandar, N (1999) Viscous drag reduction using riblets on a swept wing. AIAA Journal, 37 (7). pp. 851-856. ISSN 0001-1452
Sundaram, S and Viswanath, PR (1992) Study on turbulent drag reduction using riblets on a flat plate. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaram, S and Viswanath, PR and Rudrakumar, S (1994) Studies of turbulent. Drag reduction using riblets on a NACA 0012 aerofoil. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sundaram, S and Viswanath, PR and Rudrakumar, S (1996) Viscous drag reduction using riblets on NACA 0012 airfoil to moderate incidence. AIAA Journal, 34 (4). pp. 676-682.
Sundaram, S and Viswanath, PR and Subaschandra, N (1998) Studies on Drag Reduction Using Riblets on a Infinite Swept Wing. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sundaram, S and Yajnik, KS (1992) Experimental study on the evolution of a wall layer from a wake. AIAA Journal, 30 (12). pp. 2845-2851.
Sundaram, S and Yajnik, KS (1990) Experiments on the turbulent boundary layer on a flat plate in the wake of another flat plate. Technical Report. Experimental Aerodynamics Division, Bangalore, India.
Sundaram, S and Yajnik, KS (1990) The evolution of turbulent wall layer from free shear layer 13; 13;. In: 12th Symposium on Turbulence, 24-26 Sept 1990, United States.
Sundaramurthy, H (2005) Method for static divergence analysis of sting-mounted wind tunnel models. Technical Report. National Aerospace laboratories, Bangalore, India.
Sundaramurthy, H (1983) Review of scaling requirements for wind tunnel model for dynamic investigations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaramurthy, H (1983) Review of scaling requirements for wind tunnel models for dynamic investigations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaramurthy, H (2009) Statistical analysis of repeat test results for assessment of wind tunnel data quality. In: National Conference on Wind Tunnel Testing (2009-IT2), 12-14 Mar 2009, IISc., Bangalore.
Sundaramurthy, H (1978) Validity of axis transfer technique for pitch damping measurements AIAA-78-833. In: 10th Aerodynamic Testing Conference.
Sundaramurthy, H and Gurjale, AK and Gopala, KV (1971) Description and calibration of the 2quot;x10quot; induction tunnel (with and without plenum chamber suction). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaramurthy, H and Jategaonkar, RV and Rao, Prasada K and Vasudeva, NS (1978) A forced-oscillation rig for dynamic stability measurements in NAL high speed wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaramurthy, H and Narayana, T (1976) A free-oscillation test rig for pitch-damping measurements in N.A.L. trisonic wind tunnels. Journal of Aeronautical Society of India, 28. pp. 227-230.
Sundaramurthy, H and Prasada Rao, K (1976) A half model free oscillation fot pitch damping measurements. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Sundaramurthy, H and Suryanarayana, GK (1987) Wind tunnel simulation of PSLV strap-on booster separation trajectories. Project Report. National Aerospace Laboratories, Bangalore.
Sundaramurthy, H and Suryanarayana, GK (1985) An experimental study of multi-booster separation Aerodynamics on a 1/40 scale PSLV model. Project Report. National Aerospace Laboratories, Bangalore.
Sundaramurthy, H and Suryanarayana, GK and Lochan, R and Sivaramakrishnan, AE and Pandian, S (1995) Wind tunnel simulation of multibooster separation trajectories of a launch vehicle. Journal of Spacecraft and Rockets, 32 (3). pp. 561-563.
Sundaramurthy, H and Verma, RS and Jagadeeswarachar, SP and Kumar, Rajan (2001) Flow quality improvements in a blowdown wind tunnel 13; 13;. Journal of Aircraft, 38 (3). pp. 577-580.
Sunithamma, J and Nair, RU and Jha, RM (2004) Optimization of high performance constant thickness radome for Aerospace vehicles13;. IEEE Antennas and Propagation Society, 1. pp. 870-873.
Suresh, S and Naidu, VPS (2021) Gearbox Health Condition Monitoring Using DWT Features. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Suriyanarayanan, P and Madhavan, KT and Shailesh, Kumar and Sajeer, Ahmed Aerodynamic characteristics of Eppler 61 airfoil at Low Reynolds numbers. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, 2009,, Bangalore, India.
Suriyanarayanan, P and Venkatakrishnan, L PIV Measurements on an Air Blast Atomizer. In: 12th Asian Congress of Fluid Mechanics, 18-21 August 2008, Daejeon, Korea.
Suryanarayana, BG (1974) Design of a sidewall mounted model injection system for the NAL 1x2019; x 1x2019; trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Suryanarayana, BG (1988) Effect of ASB-II bombs and 800 litre drop tank on the aerodynamic characteristics of MiG-21 (M) aircraft. Project Report. National Aerospace Laboratories, Bangalore.
Suryanarayana, BG (1974) Some design considerations for a transient load protection system for aeroelastic testing of rocket models in the NAL blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Suryanarayana, GK (1986) Proposal for a project on powered hang gliding. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Suryanarayana, GK and Dubey, R (2017) Image analyses of supersonic air-intake buzz and control by natural ventilation. Journal of Visualization. pp. 1-17. ISSN 1875-8975
Suryanarayana, GK and Radhakrishna, SR and Srikantan, KV (1985) Calibration of NAL 3/4 inch 5-component balance for PSLV and ASLV booster separation studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Suryanarayana, G.K. and Dubey, R. (2017) Image analyses of supersonic air-intake buzz and control by natural ventilation. Journal of Visualization, 20 (4). pp. 711-727. ISSN 13438875
Suryanarayana, GK and Kurade, RB and Singh, DB and Raya, V and Kumar, S and Nath, B (2021) Trigger mechanism for obtaining dynamic derivatives in wind tunnels using free-oscillation technique. AIAA International.
Swaminadham, M (1977) Study of the vibrations of rotating blades. In: Design Engineering Technical Conference of American Society of Mechanical Engineers, 26-30 Sep 1977, Chicago, USA.
Swamy, KMM and Senthil Kumaran, R (2009) ESTIMATION OF TURBOMACHINERY FLOW LOSSES THROUGH CASCADE TESTING. In: LOSS MECHANISMS IN STEAM AND GAS TURBINES, 17-07-2009 to 18-07-2009, M.S.Ramiah School of Advanced Studies, Bangalore, India.
Swamy, MS and Ahmed, Sajeer and Sreenath, GS (1978) Model support system interference on zero-lift drag at transonic speeds. In: 10th Conference on Aerodynamic Testing, 19-21 Apr 1978, California, USA.
Swamy, Shivakumara M (1977) External store drag optimization studies at high speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Swamy, Shivakumara M (1988) Wind tunnel testing of high blockage models. Journal of Aeronautical Society of India, 40. pp. 119-130.
Swamy, Shivakumara M and Dutta, AC and Ahmed, Sajeer (1977) Experimental studies on a two-dimensional supersonic mixed compression air intake at mach numbers of 0.76, 1.06, and 1.18. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Swamy, Shivakumara M and Narasimhan, TM and Narayan, KY and Murthy, HS and Rajendra, G and Kanagarajan, V (1985) Semi-Captive Trajectory Technique. Project Report. National Aerospace Laboratories, Bangalore.
Tewari, Ashish (1993) Nonplanar doublet-point method for supersonic unsteady aerodynamics. In: 34th AIAA/ASME Adaptive Structures Forum, 19-22 Apr 1993, La Jolla, USA.
Tewari, SK (1993) Analysis of Kappatagudda main ridges wind velocity data of 1989-92. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Tewari, SK (1990) On Achieving 5000 MW from wind power. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Tewari, SK Promising high wind sites in Chitradurga Hills. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Tewari, SK (1993) Windmill rotor power regulation through self actuated leading edge spoiler. Technical Report. National Aerospace Laboratories, Bangalore, India.
Tewari, SK and Samraj, AC (1985) A brief report on the scheme for revised door numbers for Bangalore City. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Tewari, SK and Sapre, AV and Veeraraghavalu, VM (1989) Report on visit to windmill test station in Europe. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Thomas, Jim and Viji, M and Jagadeesh, G (2011) Dielectric barrier discharge for aerodynamic flow control. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Thomas, Moncy T (2001) Conceptual study of a quad tree LOD management for visual simulation13;. Technical Report. National Aerospace Laboratories, Bangalore, India.
Thulasi Durai, D and Viswamurthy , SR and Byji, Varughese and Dayananda, GN and Subrahmanya, MB and Kulkarni, DS and Rajani, BN and Mathur, JS (2009) Optimized construction of a composite MAV wing using CFD analysis. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), 10-12 December 2009, Bangalore.
Tulapurkara, EG (1987) Introduction to turbulence models and prediction of turbulent flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Upadhya, AR and Somashekar, BR (1984) Review of Launch Vehicle Related Aeroelastic Instability Studies at HAL. In: Analysis of Structures - A Commemorative volume published on the occasion of the 60th Anniversary of Dr. S.R.Valluri, Dec 1984, NAL, Bangalore, India.
Ushadevi, S and Balasingh, C (1993) Retained Austenite in Garret Engine Gears. Technical Report. National Aerospace Laboratories, Bangalore, India.
Ushadevi, S and Singh, AK (1993) Estimation of the Phases of Silicon Carbide and Silicon nitride by the X-ray Diffraction Method. Technical Report. National Aerospace Laboratories, Bangalore, India.
Vaitheeswaran, SM and Narasimhan, SV (2006) Multiresolution time domain scheme using a filter approach13;. In: 2006 International Symposium on IEEE Antennas and Propagation Society, 2006, Bangalore, India.
Vanaja, A and Rao, RMVGK (2002) Synthesis and characterisation of epoxy-novolac/bismaleimide networks. European Polymer Journal, 38 (1). pp. 187-193.
Varute, PT (1970) Setting up hydraulic/pneumatic systems facility at National Aeronautical Laboratory. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Varute, PT and Eashwar, T and Srinivasa, A and Balakrishna, S (1976) Development of quick acting valve for plot hypersonic wind tunnel of Indian Institute of Science, Bangalore. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Varute, PT and Nandakishore, KN and Vaidya, Sanjay (1992) Airworthiness Requirements for Type Certification of NALLA Report No. 3- Dynamic Tests and Analysis). Project Report. National Aerospace Laboratories, Bangalore.
Varute, PT and Nandakishore, KN and Vaidya, Sanjay (1992) Airworthiness Requirements for Type Certification of NALLA (Report No. 2-Static Tests). Project Report. National Aerospace Laboratories, Bangalore.
Varute, PT and Nandakishore, KN and Vaidya, Sanjay (1992) Airworthiness Requirements for Type Certification of NALLA (Report No.10-Cockpit Instruments/Controls Layout and Ground Calibration/Tests). Project Report. National Aerospace Laboratories, Bangalore.
Varute, PT and Nandakishore, KN and Vaidya, Sanjay (1992) Airworthiness Requirements for Type Certification of NALLA (Report No.4 - Fuselage Design/Analysis). Project Report. National Aerospace Laboratories, Bangalore.
Varute, PT and Nandakishore, KN and Vaidya, Sanjay (1992) Airworthiness Requirements for Type Certification of NALLA (Report No.6-Powerplant). Project Report. National Aerospace Laboratories, Bangalore.
Veena, S and Narasimhan, SV (2007) Laguerre escalator lattice and feedforward/feedback active noise control13;. Signal Processing, 87 (4). pp. 725-738.
Veena, S and Narasimhan, SV (2003) Performance of a Laguerre escalator based active noise control in a nonstationary environment. In: IEEE Region 10 Annual International Conference (TENCON), 15-17 Oct 2003, Bangalore, India.
Veera Sesha Kumar, C and Vivek, EK and Vignesh, K (2021) Rotordynamic Analysis and Redesign of High-Pressure Turbine Test Rig. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Veeraraghavalu, VM and Shenoy, Kalpana S (1989) Wind speed data collected in the ridge line around Talacauvery in Western Ghats during the interval October - December 1988. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Venkat Iyengar, S and Sathiyamoorthy, K and Srinivas, J and Manjunath, P (2013) Drop size characteristics of forward angled injectors in subsonic cross flows. In: Proceedings of the ASME 2013 Gas Turbine India Conference (GTINDIA2013), 5-6 Dec 2013, Bangalore, Karnataka, India.
Venkatakrishnan, L (2003) Application of resection for PSP image alignment. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2004) Comparative Study of Different Pressure-Sensitive-Paint13; Image Registration Techniques. AIAA Journal, 42 (11). pp. 2311-2319. ISSN 0001-1452
Venkatakrishnan, L (2005) Density Measurements in the Base Flow Region of HRV Afterbody-Nozzle Configuration. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2005) Development of Matlab software modules for Surface Particle Image Tracking. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2009) Development of a Novel Optical Flow Diagnostic Technique for Simultaneous Measurement of Velocity and Density in Fluid Flow with Density Gradients. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2003) Development of a Quantitative Schlieren Technique: BOS. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2004) Development of a Quantitative Schlieren Technique: BOS. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L Investigation of high-lift flows using 2D PIV. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L (2011) The Need and Impetus toward more Non-Intrusive Measurements in Indian Wind Tunnels. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011) November 2011, Bangalore, India..
Venkatakrishnan, L (2009) Recent progress in flow diagnostics techniques and aeroacoustics at NAL. In: National Conference on Wind Tunnel Testing (2009-IT10), 12-14 Mar 2009, IISc., Bangalore.
Venkatakrishnan, L and Elavarasan, R and Krothapalli, A (2000) Forward flight effects on fan noise from supersonic 2-D inlets. In: AIAA, Aerospace Sciences Meeting and Exhibit,38th, 10-13 Jan 2000, Reno, United States.
Venkatakrishnan, L and Mathur, NB (2006) PIV Studies in Under Expanded Supersonic Jets. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L and Meier, GEA (2004) Density measurements using the Background Oriented13; Schlieren technique. Experiments in Fluids, 37 (2). pp. 237-247. ISSN 0723-4864
Venkatakrishnan, L and Sundaram, S and Viswanath, PR (2006) Hysteresis and broad flow features on a Swept Wing at high lift. Journal of Aircraft, 43 (4). pp. 1036-1043. ISSN 001-8669
Venkatakrishnan, L and Sundaram, S and Viswanath, PR Observations of hysteresis and broad flow features on a swept wing at high-lift. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L and Suriyanarayanan, P (2009) Density field of supersonic separated flow past an afterbody nozzle using tomographic reconstruction of BOS data. Experiments in Fluids. pp. 463-473. ISSN 0723-4864
Venkatakrishnan, L and Suriyanarayanan, P and Madhavan, KT (2007) PIV Studies on Kaveri Fuel Injector: Phase I. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L and Suriyanarayanan, P and Mathur, JS (2009) Measurement of the three- Dimensional density field around an elliptic cone at Mach 2.0 using the BOS Technique. Project Report. National Aerospace Laboratories, Bangalore.
Venkatakrishnan, L and Suriyanarayanan, P and Mathur, NB (2007) BOS Density Measurements in Afterbody Flows with Shock and Jet Effects. In: 37th AIAA Fluid Dynamics Conference and Exhibit 25-28 , June 2007, Miami, FL.
Venkatakrishnan, L and Verma, SB (2006) Aeroacoustics instrumentation and noise measurements Part II: Propeller noise measurements. Project Report. National Aerospace Laboratories, Bangalore.
Venkatanarayana, AR and Kailash, K (1990) Rotor of a wind pump for use in shallow well salt farming at Tuticorin - A design exercise. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Venkataraman, R (1964) Mixing of dissimilar fluids in an ejector pump. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Venkatasubramanyam, DV and Ningaiah, - and Srinivasa, CR and Seshadri, BR and Ramakrishna Rao, BV (1992) Design of 1 :7 .645 scale LCA high speed air intake model. Project Report. National Aerospace Laboratories, Bangalore.
Venkatesh, TN and Mathew, J and Nanjundaiah, Ravi S (2014) Secondary instability as a possible mechanism for clear-air turbulence: a case study. Meteorology & Atmospheric Physics, 126 (3/4). pp. 139-160.
Venkiteshwaran, SP (1964) Observations in India of turbulence in the upper air from sounding balloon ascents. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Venkiteshwaran, SP and Sivaraman, KR and Gupte, CG (1965) A notice on the feasibility of wind generation of electric power for communication links in India13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Venugopal, S and Krishna Murthy, M (1989) A computer code based on experimental database to estimate the fin alone normal force characteristics upto high angles of attack. Project Report. National Aerospace Laboratories, Bangalore.
Venugopal, S and Krishnamurthy, M (1992) Missile aerodynamics at high angles of attack (MAHAA) - a prediction code. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Vepa, Ranjan (1978) Role of aeroelasticity in helicopter design. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Vepa, Ranjan and Panda, Brahmananda (1981) Rapid analysis of flap-lag vibrarions and stability of model helicopter blades. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Verma, SB and Channa Raju, - and Manisankar, C (2010) Shock-wave boundary-layer interaction study on a 20 deg compression corner using PSP and Kulites. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Manisankar, C (2009) HSTDV Nozzle Contour Optimization for Enhanced Force Characteristics – Phase I. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Manisankar, C and Akshara, P (2013) Study of Shock-Wave Boundary-Layer Interaction Control Using an Array of Steady Micro-Jet Actuators. In: NCWT-03, 2013-08-23, VSSC, Trivandrum.
Verma, SB and Manisankar, C and Channa Raju, - (2012) Control of shock unsteadiness in shock boundary-layer interaction on a compression corner using mechanical vortex generators. Shock Waves, 22. pp. 327-339.
Verma, SB and Raju, Channa and Manisankar, C (2011) Shock-Wave Boundary-Layer Interaction Study on a 20' Compression Corner Using PSP and Kulites. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Stark, R and Genin, C and Haidn, O (2011) Cold gas dual-bell tests in high-altitude simulation chamber. Shock Waves, 21. pp. 131-140.
Verma, SB and Stark, R and Haidn, O (2011) Gas density effects on dual-bell transition behavior. In: 4th European Conference for AeroSpace Sciences (EUCASS), 4-8 Jul. 2011, St. Petersburg, Russia.
Verma, SB and Stark, R and Nuerenberger-Genin, C and Hakin, O (2010) Cold-gas experiments to study the flow separation characteristics of a dual-bell nozzle during its transition modes. Shock Waves, 20. pp. 191-203.
Verma, SB and Sudhakar, and Venkatakrishnan, L (2009) Experimental study on a jet issuing from an elliptic nozzle with cylindrical tabs. Journal of Turbulence, 11 (20). pp. 1-24.
Verma, SB and Viji, M (2009) Experimental Evaluation of Linear Plug Nozzle Flow-field. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Viji, M (2011) Freestream effects on base pressure development of an annular plug nozzle. Shock Waves, 21 (2). pp. 163-171.
Verma, S.B. and Hadjadj, A. and Haidn, O, (2017) Origin of side-loads in a subscale truncated ideal contour nozzle. Aerospace Science and Technology, 71. pp. 725-732. ISSN 12709638
Verma, S.B. and Manisankar, C. (2017) Control of a Mach reflection-induced interaction using an array of vane-type vortex generators. Shock Waves. pp. 1-14. ISSN 09381287
Verma, S.B. and Manisankar, C. (2018) Control of incident shock-induced separation using vane-type vortex-generating devices. AIAA Journal, 56 (4). pp. 1600-1615. ISSN 00011452
Verma, SB and Hadjadj, A and Haidn, O (2015) Unsteady flow conditions during dual-bell sneak transition. Journal of Propulsion and Power, 31 (4). pp. 1175-1183. ISSN 07484658
Verma, SB and Haidn, OJ (2021) Effect of throttling on dual-bell sneak-transition side loads. Journal of Propulsion and Power, 37 (4). pp. 634-644. ISSN 07484658
Verma, SB and Manishankar, C (2015) Transition control of Mach to regular reflection induced interaction using an array of micro ramp vane-type vortex generators. Physics of Fluids, 27 (10). ISSN 10706631
Vijayashankar, CS and Srinivasamurthy, R and Prem Singh, M (1985) General specifications for a captive power driven compressors and dryer system. Project Report. National Aerospace Laboratories, Bangalore.
Viji, M and Sathia Narayanan, A and Mathur, NB (2013) Aerodynamic performance evaluation of twinjet afterbody using flow through balance. In: National conference on wind tunnel testing, 2013-08-23, Thiruvananthapuram.
Viji, M and Vikramaditya, NS (2019) Modes of base pressure fluctuations: Shape, nature, and origin. AIAA Journal, 57 (9). pp. 3933-3942. ISSN 00011452
Vikramaditya, N.S. and Viji, M (2019) Mach Number Effect on Symmetric and Antisymmetric Modes of Base Pressure Fluctuations. Journal of Fluids Engineering, Transactions of the ASME, 141 (2). ISSN 00982202
Vikramaditya, N.S. and Viji, M. and Verma, S.B. and Ali, N. and Thakur, D.N. (2018) Base pressure fluctuations on typical missile configuration in presence of base cavity. Base pressure fluctuations on typical missile configuration in presence of base cavity, 55 (2). pp. 335-345. ISSN 00224650
Vinay, CA and Bhaskar, Chakravarthy (2014) Aero-thermal Analysis of Insulation to Protect Exhaust Ducts of A Pusher Turbo Prop Engine Aircraft. In: 5th International and 41st National Conference on Fluid Mechanics and Fluid Power (FMFP-2014), 12 December 2014, IIT Kanpur.
Vinay, CA and Bhaskar, Chakravarthy and Malisetty Leela, Shankar (2014) Aero-thermodynamic Design of Jet Pump for A Turboprop Aircraft Engine in Pusher Configuration. In: 5th International and 41st National Conference on Fluid Mechanics and Fluid Power (FMFP-2014), 12 December 2014, IIT Kanpur.
Vinay Kumar, - (1989) Experimental studies on a 1/10th scale model of Agni- payload missile. Project Report. National Aerospace Laboratories, Bangalore.
Vinay Kumar, - and Sreenath, GS (1987) Wind tunnel tests on BAE R-80 Calibration Model. Project Report. National Aerospace Laboratories, Bangalore.
Vineet, Kumar (2009) Extraction of hinge-moment derivatives of rudder and its tabs (tab chord extended aft of rudder trailing edge) from flight tests of saras PT-2 aircraft. Technical Report. NAL.
Vinod Kumar, N and Prathapanayaka, R and Jai Maruthi, R and Swaroop, S (2021) 3D Finite Element Rotor Dynamic Analysis of Turbine Test Rig Rotor-Shaft Systems. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Vinod Kumar, N and Prathapanayaka, R and Jai Maruthi, R and Swaroop, S (2021) 3D Finite Element Rotor Dynamic Analysis of Turbine Test Rig Rotor-Shaft Systems. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Vishal, S Shirbhate (2012) Reynolds Averaged Navier-Stokes Analysis for Civil Transport Aircraft using Structured and Unstructured grids. In: 14th Annual CFD Symposium, 10 Aug 2012, IISC, Bangalore.
Viswanath, PR (2002) Aircraft viscous drag reduction using riblets. Progress in Aerospace Sciences, 38 (6-7). pp. 571-600.
Viswanath, PR (1986) Buffet onset measurements on an Aircraft model at transonic mach numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath, PR Drag reduction of afterbodies by controlled separated flows. AIAA Journal, 39 (1). pp. 73-78. ISSN 0001-1452
Viswanath, PR (1996) Flow management techniques for base and after body drag reduction13;. Progress in Aerospace Sciences, 32 (2-3). pp. 79-129.
Viswanath, PR (1985) Investigation of passive devices for axisymmetric base13; drag reduction at transonic speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath, PR (1988) Passive devices for axisymmetric base drag reduction at transonic speeds. Journal of Aircraft, 25. pp. 258-262. ISSN 0021-8669
Viswanath, PR (1988) Shock-wave-turbulent-boundary-layer interaction and its control - A survey of recent developments. In: IN: Developments in fluid mechanics and space technology (A89-50001 22-34, Bangalore,India.
Viswanath, PR (1995) Vortex asymmetry and induced side forces on elliptic cones at high incidence. Journal of Aircraft, 32 (5). pp. 1018-1025.
Viswanath, PR (1985) A project proposal for high angle of attack aerodynamic characteristics of wing-body combinations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath, PR (1985) A project proposal for high angle of attack aerodynamic13; characteristics of wing-body combinations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath, PR and Narayan, KY (1985) Side force characteristics of A 20 deg. cone at high angles of attack. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath, PR and Patil, SR (1994) Aerodynamic characteristics of delta wing-body combinations at high angles of attack. Aeronautical Journal, 98 (975). pp. 159-170.
Viswanath, PR and Patil, SR (1994) Aerodynamic characteristics of delta wing-body combinations at high angles of attack. Aeronautical Journal, 98 (975). pp. 159-170. ISSN 0001-9240
Viswanath, PR and Patil, SR (1988) Performance of passive devices for axisymmetric base drag reduction at mach 2. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath, PR and Patil, SR (1997) Zero-lift drag characteristics of afterbodies with a square base. Journal of Spacecraft and Rockets, 34 (3). pp. 290-293. ISSN 0022-4650
Viswanath, PR and Rajendra, G (1990) Sting corrections to zero-lift drag of axisymmetric bodies in transonic flow 13;. Aeronautical Journal, 94. pp. 279-288.
Viswanath, PR and Rajendra, G (1989) Sting-support interference on afterbody drag at transonic speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanath , PR (1985) Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal. Project Report. National Aerospace Laboratories, Bangalore.
Viswanatha Rao, AN and Naidu, VPS and Jana, S (2021) Gas Turbine Engine Fan Blade Flutter Detection Using Casing Vibration Signals by Application of Recurrence Plots and Recurrence Quantification Analysis. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
Viswanathan, R and Baghialakshmi, S (1974) Voltage controlled two phase func generator using op-amps. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanathan, R and Murthy, Diwakara HS (1982) A twin-axis vibration pick up. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanathan, R and Raghu, M (1986) Vibration measurements made in LSI laboratory, Indain Telephone Tndustries. Project Report. National Aerospace Laboratories, Bangalore.
Viswanathan, S (1970) Programs to analyze supersonic flow past right circular cones with a view to make use of uncalibrated cones for determination of flow angles and mach numbers in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Viswanathan, S and Narayana, CL and Ramesh, V and Desai, SS and Rangarajan, R (1993) Panel codes for aerodynamic analysis at NAL. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.
Vivek, EK and Lakshya Kumar, - and Senthil Kumaran, R and Veera Sesha Kumar, C (2021) Improving Structural Integrity of a Centrifugal Compressor Impeller by Blading Optimization. In: Proceedings of the 6th National Symposium on Rotor Dynamics, Singapore.
William Grips, VK and Ezhil Selvi, V and Barshilia, Harish C and Rajam, KS (2005) Effect of electroless nickel interlayer on the electrochemical behavior of single layer CrN, TiN, TiAlN coatings and nanolayered TiAlN/CrN multilayer coatings prepared by reactive dc magnetron sputtering. Electrochimica Acta, 51 (17). pp. 3461-3468.
Wind Energy Programme, (1999) Wind resource assessment in Atankari Pallivasal, Thirunelveli District Tamilnadu. Technical Report. National Aerospace Laboratories, Bangalore, India.
Wind Energy Programme, (1999) Wind resource assessment in Athukuruchi, Thirunelveli district, Tamilnadu. Technical Report. National Aerospace Laboratories, Bangalore, India.
Wind Energy Programme, (1999) Wind resource assessment in Dharapuram, Coimbatore District, Tamilnadu. Technical Report. National Aerospace Laboratories, Bangalore, India.
Wind Energy Programme, (1999) Wind resource assessment in Karamadai, Coimbatore District, Tamilnadu. Technical Report. National Aerospace Laboratories, Bangalore, India.
Wind Energy Programme, (1999) Wind resource assessment in KulliaPalayam, Coimbatore District, Tamilnadu. Technical Report. National Aerospace Laboratories, Bangalore, India.
Wind Energy Programme, (1999) Wind resource assessment in Kuttam, Thirunelveli District, Tamilnadu. Technical Report. National Aerospace Laboratories, Bangalore, India.
Wind Energy Programme, (1997) Wind speed data at Sogi B near Harapanahalli for the period June 1996 to March 1997. Technical Report. National Aerospace Laboratories, Bangalore, India.
Winson, D and Choudhury, Balamati and Selvakumar, N and Barshilia, Harish C and Nair, RU (2019) Design and Development of a Hybrid Broadband Radar Absorber Using Metamaterial and Graphene. IEEE Transactions on Antennas and Propagation, 67 (8). pp. 5446-5452. ISSN 0018926X
Yadav, R and Jugseniya, Chandrakant B and Pashilkar, AA (2005) Thermodynamic analysis of turbofan engine. In: ASME Turbo Expo 2005: Power for Land, Sea, and Air (GT2005) , June 6–9, 2005, Reno, Nevada, USA .
Yadav, R and Kapadi, Yogesh and Pashilkar, AA (2005) Aero-thermodynamic model for digital simulation of turbofan engine. In: ASME Turbo Expo 2005: Power for Land, Sea, and Air (GT2005) , June 6–9, 2005 , Reno, Nevada, USA.
Yajnik, KS (1975) Energy turn rate characterstic of an aircraft and turn performance. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Yajnik, KS (1984) Turbulent boundary layers perturbed by embedded bodies. In: 2nd Asian Congress of Fluid Mechanics, 25--29 October, 1983, Beijing, China.
Yajnik, KS and Acharya, M (1978) Non-equilibrium effects in a turbulent boundary layer due to the destruction of large eddies. In: Proceedings of the Symposium on Turbulence, Structure and Mechanisms of turbulence I, 1-5 Aug 1977, Berlin, Germany.
Yajnik, KS and Subbaiah, MV (1973) Experiments on swirling turbulent flows. I - Similarity in swirling flows. Journal of Fluid Mechanics, 60 (4). pp. 665-687.
Yajnik, KS and Subbaiah, MV (1975) On the representation of the drag polar of a fighter aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Yajnik, KS and Subbaiah, MV (1976) Representation of the drag polar of a fighter aircraft. Journal of Aircraft, Vol. 1. pp. 155-156. ISSN 0021-8669
Yanamashetti, Gireesh and Murthy, Sundara H (2011) Application of Global Regression Method for Calibration of Wind Tunnel Balances. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Yanamashetti, Gireesh and Murthy, Sundara H (2011) Application of global regression method for calibration of wind tunnel balances. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
Yegna Narayan, K and Seshadri, SN (1995) Types of Flow on the Lee Si-de of Delta Wings. Technical Report. National Aerospace Laboratories, Bangalore, India.
Yegna Narayan, K and Seshadri, SN (1997) Types of flow on the lee side of delta wings. Progress in Aerospace Sciences, 33 (3-4). pp. 167-257. ISSN 0376-0421
Zebiri, B and Piquet, A and Hadjadj, A and Verma, SB (2020) Shock-induced flow separation in an overexpanded supersonic planar nozzle. AIAA Journal, 58 (5). pp. 2122-2131. ISSN 00011452
