Items where Subject is "ENGINEERING > Fluid Mechanics and Thermodynamics"

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Number of items at this level: 495.

Ramesh, V (2002) Least squares grid free kinetic upwind method. ["eprint_fieldopt_thesis_type_phd" not defined] thesis, Indian Institute of Science, Bangalore.

A

Abdul Huq, A and Anand Sankar, R and Lakshmanan, C and Rukesh, C and Kulkarni, DS and Subramanya, MB and Rajani, BN (2009) Numerical Prediction of Aerofoil Aerodynamics at Low Reynolds number for MAV Application. Project Report. National Aerospace Laboratories, Bangalore.

Ailneni, S and Kashyap, SK and Kumar, NS (2016) Real time sensor fusion for micro aerial vehicles using low cost systems. In: 2015 10th Asian Control Conference: Emerging Control Techniques for a Sustainable World, ASCC 2015, 4-6 June 2016, Hyderabad, India.

Alone, DB and Kumar, SS and Shobhavathy, MT and Mudipalli, JRR and Pradeep, AM and Ramamurthy, S and Iyengar, VS (2017) Experimental assessment on effect of lower porosities of bend skewed casing treatment on the performance of high speed compressor stage with tip critical rotor characteristics. Aerospace Science and Technology, 60. pp. 193-202. ISSN 12709638

Anand, Kumar (1987) Euler calculations for lca configurations (Draft Project Proposal). Project Report. National Aerospace Laboratories, Bangalore.

Anantha, KV and Mathur, NB and Krishnan, V (1989) Design characteristics of the variable supersonic nozzle of the base flow facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Arivoli, D and Singh, Ishan (2016) Self-adaptive flaps on low aspect ratio wings at low Reynolds numbers. Aerospace Science and Technology, 59. pp. 78-93. ISSN 12709638

Arivoli, D and Singh, Ishan and Suriyanarayanan, P (2017) PIV investigation of self-adaptive flap on low aspect ratio wings. In: AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, 9 - 13 January 2017, Grapevine, Texas.

Asokan, K and Anil Kumar , CV and Dasan, J and Radhakrishnan, K and Satheesh Kumar, K and Ramamohan, TR (2005) Review of chaos in the dynamics and rheology of suspensions of orientable particles in simple shear flow subject to an external periodic force. Journal of Non-Newtonian Fluid Mechanics, 129. pp. 128-142.

Asokan, K and Ramamohan, TR (2004) The rheology of a dilute suspension of Brownian dipolar spheroids in a simple shear flow under the action of an external force. Physics of Fluids, 16 (2). pp. 433-444. ISSN 1070-6631

B

Balakrishna, S and Niranjana, T and Rajamurthy, MS and Srinathkumar, S and Rajan, SR and Singh, Suresh K (1993) Estimation of aerodynamic derivatives using Dynamic Wind Tunnel Simulation Technique. In: Symposium on System identification, 24-25 Nov 1993, Bangalore, India.

Bandyopadhyay, K (1992) Determination of Aerodynamic flow transition using piezoelectric polymer foil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Basu, AJ (1994) CFD on parallel computers. In: CFD: Advances and Applications, India.

Basu, AJ (1994) Spectral methods for fluid flow. In: CFD: Advances and Applications, 1994, India.

Basu, AJ and Sinha, UN and Narasimha, R (1992) Direct Numerical Simulation of Turbulence on the Flosolver MK3 Parallel Computer. Technical Report. National Aerospace Laboratories, Bangalore, India.

Bekinal, SI and Jana, S (2016) Generalized three-dimensional mathematical models for force and stiffness in axially, radially, and perpendicularly magnetized passive magnetic bearings with "n" number of ring pairs. Journal of Tribology, 138 (3). ISSN 07424787

Bera, Rajendra K (1990) Accurate method for calculating initial development of vortex sheets. Journal of Aircraft, 27. pp. 910-912. ISSN 0021-8669

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 (1994) Comment on quot;quot;Computational13; Challenge: Euler Solution for Ellipsesquot;quot;. Technical Report. National Aerospace Laboratories, Bangalore, India.

Bera, Rajendra K (1989) Design priorities for an air-superiority fighter. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1989) Design priorities for an air-superiority fighter. Journal of Aeronautical Society of India, 41. pp. 407-411.

Bera, Rajendra K (1988) Design priorities for an air-superiority fighter. In: 40th Annual General Meeting, 19-20 Dec 1988, Madras, India.

Bera, Rajendra K (1990) Do inviscid vortex sheets roll-up? Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1990) Flow past a lifting arc. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1992) On Shankar's Counterexample to Lighthill's Lemma. Technical Report. National Aerospace Laboratories, Bangalore, India.

Bera, Rajendra K (1989) On the dynamics of point vortices. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1975) On the wave drag integral for slender bodies. Journal of Aircraft, 12 (11). pp. 908-910. ISSN 0021-8669

Bera, Rajendra K (1994) Quadrature Rule for a Double-pole Singular Integral. Technical Report. National Aerospace Laboratories, Bangalore, India.

Bera, Rajendra K (1988) Quadrature formula for a double-pole singular integral ((in linear lifting surface theory). AIAA Journal, 26. pp. 752-754. ISSN 0001-1452

Bera, Rajendra K (1987) A Quadrature formula for a double-pole singular integral. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1990) The lifting line equation - Revisited. Technical Report. National Aeronautical Laboratory, Bangalore, India.

C

Chakrabartty, SK (1992) Approximate factorization scheme for transonic potential flow computations. Sadhana, 17 (2). pp. 299-313. ISSN 0256-2499

Chakrabartty, SK (1989) Computation of transonic potential flow RAE-wing-A and body-B2 combination. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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 (1994) Computation of viscous transonic flows with shocks. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K (1992) A Vertex based finite volume algorithm for three dimensional navier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, JS (1994) Computation of Three- Dimensional Transonic Flow Using a Cell Vertex Finite Volume Method for the Euler Equations. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, JS (1998) Euler Analysis of SARAS Wing-fuselage Configuration. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, JS (1996) Navier-Stokes Analysis of Vortex Flow Over a13; Cropped Delta Wing. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Mathur, S (1994) Euler Computation for a Multi-Body Launch Vehicle. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chakrabartty, SK and Dhanalakshmi, K and Ramesh, V (2003) Navier-stokes analysis of GA(W)-2 aerofoil with deflected flap and redesign of Hansa flap for better performance. Computational Fluid Dynamics Journal, 12 (1). pp. 89-97. ISSN 0918-6654

Chakrabartty, SK and Subramanian, NR (1988) Computation of 3-D transonic flows for wings and wing-body configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1989) Computation of 3-D transonic flows for wings and wing-body configurations (Closure Report)13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1989) Computation of 3-D transonic flows for wings and wing-body13; configurations (Annual Progress Report). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR (1986) Computation of transonic potential flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chakrabartty, SK and Subramanian, NR and Siddalingappa, SR and Das, AK (1987) Computation of 3-D Transonic Flow for Wings and Wing Body13; Configuration. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Chandra, Ramesh and Guruprasad, K (1987) Numerical estimation of stress intensity factors in patched cracked plates. Engineering Fracture Mechanics, 27 (5). pp. 559-569. ISSN 0013-7944

Chotalia, RJ and Alone, DB (2017) Numerical investigations on influence of uniform blade surface roughness on the performance characteristics of a transonic axial flow compressor stage. In: ASME 2017 Gas Turbine India Conference, GTINDIA 2017, 7 - 8 December 2017, Bangalore, India.

Christ, Thomas and Lathasree, P and Singh, GK and Iyer, SR (2003) Modeling and simulation of HAL Bangalore international airport. Technical Report. National Aerospace Laboratories, Bangalore, India.

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.

Chutkey, Kiran and Vasudevan, B and Balakrishnan, N (2016) Flow and performance analysis of annular cluster truncated plug nozzle. Journal of Propulsion and Power, 32 (6). pp. 1442-1453. ISSN 07484658

D

Danish, TH and Sathiyamoorthy, K and Srinivas, J and Manjunath, P (2013) Drag Characterization of Strut-mounted 'Through Cavity' for Scramjet Applications. In: 23rdNational Conference on I. C. Engine and Combustion (NCICEC 2013), 13-16 Dec 2013, SVNIT, Surat, India.

Danish, TH and Sathiyamoorthy , K and Prateesh Kumar, P and Manjunath, P (2013) Characterization of Strut-mounted ‘Through Cavity’ for Scramjet Applications. In: The 14th Asia Congress of Fluid Mechanics - 14ACFM, 15-19 Oct 2013, Hanoi and Halong, Vietnam.

Darji, AP and Alone, DB and Mistry, CS (2017) Flow studies on a single stage transonic axial flow compressor retrofitted with circumferential grooves and varied rotor-stator axial gap. In: ASME 2017 Gas Turbine India Conference, GTINDIA 2017, 7 - 8 December 2017, Bangalore, India.

Das, A and Kumar, A (1987) Numerical solution of flow fields around delta wings using euler equation method. Part II: Analysis of the results and comparison with experiments. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Das, SP and Srinivasan, U and Arakeri, JH (2016) Instabilities in unsteady boundary layers with reverse flow. European Journal of Mechanics, B/Fluids, 55. pp. 49-62. ISSN 09977546

Davis, D and Singha, Sintu and Chakradhar, RPS and Srivastava, Meenu (2020) Tribo–Mechanical Properties of HVOF-Sprayed NiMoAl-Cr2AlC Composite Coatings. Journal of Thermal Spray Technology, 29. pp. 1763-1783. ISSN 10599630

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

De, Manabendra M and Mathur, JS and Vengadesan, S (2021) 3D Computational Studies of Flapping Wing in Frontal Gusty Shear Flow. In: Design and Development of Aerospace Vehicles and Propulsion Systems, 15 June 2021, Singapore.

De, Manabendra M and Mathur, JS and Vengadesan, S (2020) On the Recurrence Signatures of Flapping Wings Exposed to Gusty Simple Shear Flow. In: Lecture Notes in Mechanical Engineering.

De, Manabendra M and Mathur, JS and Vengadesan, S (2019) Recurrence studies of insect-sized flapping wings in inclined-stroke plane under gusty conditions. Sadhana - Academy Proceedings in Engineering Sciences, 44 (3). pp. 1-17. ISSN 02562499

Deshpande, MD (1993) Basic equations of fluid dynamics. In: CFD: Advances and Applications, 9-11 Aug 1993, Bangalore, India.

Deshpande, MD (1993) Flow Regimes in a Three-Dimensional Driven Cavity13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD (1986) Laminar jet impingement on an indented wall. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD (1986) Laminar jet impingement on an indented wall. Zeitschrift fuer angewandte Mathematik und Physik (ZAMP), 37 (3). pp. 361-373.

Deshpande, MD (1992) On the selection of the stable explicit first order difference scheme13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD (1987) Power Monomial relation between parameters related by a physical law. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD (1992) Stability analysis of third order upwind difference schemes. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD and Milton, SG (1995) Computation of Kolmogorov Scales in a Driven Cavity Flow. Technical Report. National Aerospace Laboratories, Bangalore, India.

Deshpande, MD and Milton, SG (1995) Direct simulation of turbulent flow at a Reynolds number of 10,000. In: 6th Asian Congress of Fluid Mechanics, 22-26 May 1995, Singapore.

Deshpande, MD and Milton, SG and Balaji, S (1994) A detailed description of transitional and turbulent flow in a three-dimensional cavity. Technical Report. National Aerospace Laboratories, Bangalore, India.

Deshpande, MD and Murugan, M and Sinha, UN (1993) Solution of three-dimensional incompressible navier-stokes13; equations on FLOSOLVER. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD and Rao, Sanjeev K and Shankar, PN (1999) Modification and Testing of JUMBO3D Code for LES Computations. Technical Report. National Aerospace Laboratories, Bangalore, India.

Deshpande, MD and Sengupta, TK (1986) Estimation and improvement of accuracy difference schemes with algebraic transformation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD and Shankar, PN (1988) Experiments on liquid vapour phase change between plane liquid surfaces part:3 results from a closed quartz chamber. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Deshpande, MD and Shankar, PN (1994) Transitional and Turbulent13; Flow in a Three Dimensional13; Cavity. Technical Report. National Aerospace Laboratories, Bangalore, India.

Deshpande, MD and Shankar, PN (1993) The structure of laminar flow in a three-dimensional driven cavity. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 Jul 1993, Sikkim, India.

Deshpande, MD and Sinha, UN and Sarasamma, VR and Sivaramakrishnan, Rajalakshmy and Ramakrishnan, CR (1987) Solution of Airier-stokes Equations on Flowsolver Using Concurrent/Parallel Algorithm. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Deshpande, MD and Sreenivasan, CR and Sridhar, S and Sarasamma, VR (1989) Presentations at the Flosolver Workshop :27-28 December 1988. Project Report. National Aerospace Laboratories, Bangalore.

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

Dhanalakshmi, K and Mathur, JS and Chakrabartty, SK (1999) Euler Computation for a Wing with Aileron Deflection. Technical Report. National Aerospace Laboratories, Bangalore, India.

Dutta, PK (1994) Discrete vortex method for computation of viscous incompressible flows 13;. In: CFD: Advances and Applications, 1994, India.

Dutta, PK (1989) Discrete vortex simulation of high reynolds number flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, PK (1986) Discretization of rotational regions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, PK (1993) A vortex method for viscous unsteady flows. In: Proceedings of the Fluid Dynamics Symposium in honour of Prof. R. Narasimha on his 60th birthday, 9 July 1993, Sikkim, India.

Dutta, Vimala (1988) Application of Program Laws to LCA Planforms. Project Report. National Aerospace Laboratories, Bangalore.

Dutta, Vimala (1993) Computation of compressible flows: Implicit methods 13; 13;. In: CFD: Advances and Applications, 1993, Bangalore, India.

Dutta, Vimala (1985) Computational requirements for the solution of navier-stokes equations. Project Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, Vimala (1988) Implicit boundary condition procedure - Application to 1-D euler solver. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, Vimala (1988) LAWS-Lift analysis of wings in supersonic flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, Vimala (1988) Solution of one-dimensional euler-equations by the implicit finite difference technique of beam and warming. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, Vimala (1993) An implicit finite volume nodal point scheme for the solution of two-dimensional compressible 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.

Dutta, Vimala (1989) An implicit navier-stokes solver for the steady laminar supersonic flow past a semi-infinite flat plate at zero incidence. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutta, Vimala and Desai, SS (1999) Position for a Stall Warning System on HANSA-3 Prototype-II. Technical Report. National Aerospace Laboratories, Bangalore, India.

Dutta, Vimala and Dwarakanath, GS and Ramamoorthy, P (1985) Determination of an optimum trajectory for a two stage rocket13; 13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.

F

Felix, J and Rajendran, R and Kumar, GN and Babu, YG and Karthik, MK and Ramesha, DK (2019) Experimental and Numerical Investigation of Effusion Cooling Performance Over Combustor Liner Flat Plate Model. Heat Transfer Engineering, 40 (15). pp. 1-14. ISSN 01457632

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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

Giridhar, Babu Y and Ashok Babu, TP and Raghavan , R and Felix , J (2014) Experimental Investigation of Adiabatic Film Cooling Effectiveness and Heat Transfer Coefficients over a Gas Turbine Blade Leading Edge Configuration. In: 2014 International Conference on Material Science and Material Engineering [MSME2014], 15 Mar 2014, Chicago, Illinois, USA.

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 Raol, JR (1996) Asymptotic and Generalisation Theory of Equation Decoupling Method for System Parameter Estimation. Journal of the Institution of Engineers (India): Electrical Engineering Division, 77 (AUG). pp. 80-83.

Girija, G and Shantha Kumar, N (2007) Three Model IMM-EKF for tracking targets executing evasive maneuvers. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, 8-11 Jan 2007, USA.

Gopinath, PR and Sundaram, S and Madhavan, KT and Siddalingappa, SR and Yajnik, KS (1988) Flow visualisation of leading edge vortices on a Delta Wing by laser sheet technique. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R (1990) Wall interference studies (Closing Report Apr. 1983 - Jun. 1989). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R (1993) Wall interference studies: Revisited 13; 13;. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.

Gopinath, R (1991) A comparison of inviscid flow past airfoils by the full potential and euler codes. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R (1990) The tunnel interference index. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R and Vishwanathan, S and Desai, SS (1991) A numerical assessment of wall interference in 2-D 13; 13;. In: ICAW 1991: International Conference on Adaptive Wall Wind Tunnel Research and Wall Interference Correction, 10-14 Jun 1991, China.

Govindarajan, Rama (1993) Stability of spatially developing boundary layers 13;. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 Jul 1993, Sikkim, India.

Govindarajan, Rama (1992) Transition prediction from linear stability computations. Technical Report. National Aerospace Laboratories, Bangalore, India.

Govindarajan, Rama and Narasimha, R (1999) Low-order parabolic theory for 2D boundary-layer stability. Physics of Fluids, 11 (6). pp. 1449-1458. ISSN 1070-6631

Govindarajan, Rama and Narasimha, R (1993) Stability of spatially developing boundary layers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Govindarajan, Rama and Narasimha, R (1994) Stability of spatially developing boundary layers in pressure gradients. Technical Report. National Aerospace Laboratories, Bangalore, India.

Govindarajan, Rama and Narasimha, R (1997) A low-order theory for stability of non-parallel boundary layer flows. Proceedings of the Royal Society of London, Series A (Mathematical, Physical and Engineering Sciences), 453 (1967). pp. 2537-2549. ISSN 1364-5021

Govindarajan, Rama and Narasimha, R (1989) The role of residual non-turbulent disturbances on 13; transition onset in two-dimensional boundary layers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Govindarajan, Rama and Narasimha, R (1991) The role of residual nonturbulent disturbances on transition onset in two-dimensional boundary layers. Journal of Fluids Engineering, 113. pp. 147-149.

Gupta, Anurag and Dunne, Rajiv Carl and Majumdar, Sekhar (1993) Calculation of 2D compressible flows using a pressure based finite volume algorithm. Technical Report. National Aerospace Laboratories, Bangalore, India.

Gupta, Ramesh P (1974) A technique for flow measurement in separated flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.

H

Hazra, SB and Chakrabartty, SK and Niyogi, P (1999) Compressible viscous flow past aerofoils using a non-oscillatory finite-volume scheme. Computational Fluid Dynamics Journal, 8 (3). pp. 400-409.

Hebbar, KS (1986) Mean and turbulence measurements in the boundary layer and wake of a symmetric aerofoil. Experiments in Fluids, 4. pp. 214-222.

Hebbar, KS (1977) On near-wall collateral flow in skewed turbulent boundary layers. AIAA Journal, 15 (10). pp. 1509-1511. ISSN 0001-1452

Hussain, S and Poddar, S and Ailneni, S and Kumar, V and Kumar, A (2015) Tuning of Extended Kalman filter using Human Opinion Dynamics based optimization. In: 2015 International Conference on Industrial Instrumentation and Control, ICIC 2015, 28-30 May 2015, Pune, India.

J

Jaiswal, S and Mathur, JS (2017) Implementation of matrix dissipation scheme for numerical simulations of two dimensional Navier-Stokes equations. Lecture Notes in Mechanical Engineering, PartF8. pp. 343-352. ISSN 21954356

Jarali, Chetan S and Raja, S and Upadhya, AR (2010) Constitutive modeling of SMA SMP multifunctional high performance smart adaptive shape memory composite. Smart Materials and Structures, 19 (10). ISSN 0964-1726

Jayalakshmi, M and Patel, Vijay V and Singh, GK (2021) Relook at aileron to rudder interconnect. Defence Science Journal, 71 (2). pp. 153-161. ISSN 0011748X

Jayaraman, V (1987) Surface Pressure Distributions on an Axisymmetric Underwater Body - Theory and Experiment. Project Report. National Aerospace Laboratories, Bangalore.

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 of Screen elements used for a Radio Telescopic Antenna (GIMRT). 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 an Axisymmetric Body at Angles of Attack Part V - Boundary Layer Profile Measurement on an Axisymmetric Body. 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 Singh, Khem (1988) Calibration and some typical measurements in the free jet facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Jeyaseelan, AR and Poornima, N and Senthil Kumaran, R (2012) A Wireless Multichannel Pressure Measurement System for a Rotating Turbo machinery Rig. In: National Symposium on Instrumentation (NSI-37), CSIR-CSIO, Chandigarh.

Joshi, PR and Rajaei, H and Kunnen, RPJ and Clercx, HJH (2016) Effect of particle injection on heat transfer in rotating Rayleigh-Bénard convection. Physical Review Fluids, 1 (8). ISSN 2469990X

Josy, Pullockara P (2009) CFD as a design tool for small aircraft: Saras propeller aerodynamics: 1. Technical Report. NAL.

Jyothi Kumar, Puttam and Shankara Rao, Gonti (2014) Validation of Shock-Expansion Tool for Two-dimensional and Axisymmetric Flows with CFD. In: 16th AESI Annual CFD Symposium, 11 Aug 2014, CSIR-NAL, Bangalore.

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Kailas, SV and Kalavathi, K and Bhat, GS (1995) On coherent structures in a round turbulent jet educed by wavelet transforms. In: 6th Asian Congress of Fluid Mechanics, 22-26 May 1995, Singapore.

Kamali, C and Pashilkar, AA (2011) Evaluation of Recursive Least Squares algorithm for parameter estimation in aircraft real time applications. Aerospace Science and Technology, 15 (3). pp. 165-174. ISSN 1270-9638

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

Kamali, C and Ozger, E (2019) Limitations of Flight Path Reconstruction techniques. Sadhana - Academy Proceedings in Engineering Sciences, 44 (2). pp. 1-15. ISSN 02562499

Kannan, SM and Purohit, SC and Subramanian, NR (1988) Algebraic grid generation for missile-type configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Karthikeyan, N and Venkatakrishnan, L (2017) Acoustic characterization of jet interaction with launch structures during lift-off. Journal of Spacecraft and Rockets, 54 (2). pp. 356-367. ISSN 00224650

Kashyap, SK and Raol, JR (2005) Performance evaluation of derivative free Kalman filter for non-linear estimation problem. In: ICECON 05, 2005, Tiruchirappalli, Chennai, India.

Kashyap, SK and Raol, JR (2006) Soft decision fusion using kalman filter and fuzzy logic. Technical Report. National Aerospace Laboratories, Bangalore, India.

Khadeeja Nusrath, TK and Basappa, Shri and Singh, Jatinder and Babu, GK (2017) In-Flight Center-of-Gravity Estimation Using Extended Kalman Filter. In: 2016 IEEE Annual India Conference, INDICON 2016, 16 - 18 December 2016, Bangalore, India.

Khadeeja Nusrath, TK and Singh, Jatinder and Saraf, Amitabh (2016) External stores grouping for aero database update. In: AIAA Atmospheric Flight Mechanics Conference, 4-8 January 2016, San Diego, California, USA.

Khan, AA and Shembharkar, TR (2004) Computation of High Speed Cold Cavity Flow with a Commercial CFD Code. In: 31st National Conference on Fluid Mechanics & Fluid Power, 16-18 Dec 2004, Jadavpur University, Kolkata, India.

Khan, AA and Shembharkar, TR (2008) Numerical Simulation of Supersonic Combustion in a Slant Cavity. In: 10th Annual CFD Symposium, 11-12 Aug 2008, NAL, Bangalore, India.

Kidambi, R (2009) Capillary damping of inviscid surface waves in a circular cylinder. Journal of Fluid Mechanics, 627. pp. 323-340.

Kidambi, R (2011) Frequency and damping of non-axisymmetric surface oscillations of a viscous cylindrical liquid bridge. Journal of fluid Mechanics, 681. pp. 597-621.

Kidambi, R (2007) Meniscus effects on the frequency and damping of capillary-gravity waves in a brimful circular cylinder. Technical Report. National Aerospace Laboratories, Bangalore, India.

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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.

Kumar, A and Sudharsan, R (1993) Calculation of vortex flow on a delta wing. Technical Report. National Aerospace Laboratories, Bangalore, India.

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Kumar, A Ashok and Alagar, M and Rao, RMVGK (2001) Studies on thermal and morphological behavior of Siliconized Epoxy Bismaleimide Matrices. Journal of Applied Polymer Science, 81. pp. 2330-2346.

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Kumar, Anand (1993) Navier-stokes simulation of transonic vortex flow over a delta wing. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.

Kumar, Anand (1987) Preliminary viscous flow calculation past a wing using navier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore.

Kumar, Anand (1987) Preliminary viscous flow calculation past a wing using navier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kumar, Anand (1985) A contour plot program. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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Kumar, Manoj and Arakeri, JH and Shankar, PN (1994) A Note on Translational Velocity Oscillations of Piston Generated Vortex Rings. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kumar, Manoj and Shankar, PN (1995) New vortex ring translational instability. In: 6th Asian Congress of Fluid Mechanics, 22-26 May 1995, Singapore.

Kumar, NS and Kumar, A (1987) Grid Generation by optimisation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kumar, SR and Narasimha, R and Prabhu, A (1995) Structure of momentum and heat flux events in the atmospheric surface layer. In: 6th Asian Congress of Fluid Mechanics, 22-26 May 1995, Singapore.

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Kumar, Sunil C and Gopalratnam, Girija (1991) Graphics for interactive PC based parameter estimation package. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kumar, A and Manoj, N and Onkar, AK and Manjuprasad, M (2016) Fluid-Structure Interaction Analysis of a Cropped Delta Wing. In: Procedia Engineering}.

Kumar, SS and Kandagal, SB and Ganguli, Ranjan and Jana, S (2017) Structural dynamic behavior of axial compressor rotor. In: ASME 2017 Gas Turbine India Conference, GTINDIA 2017, 7 - 8 December 2017, Bangalore, India.

Kumaran, RS and Kumar, K and Poornima, N (2017) Experimental study of unsteady pressure fluctuations due to tip leakage flows in an axial flow turbine. In: ASME 2017 Gas Turbine India Conference, GTINDIA 2017, 7 - 8 December 2017, Bangalore, India.

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Madhukar, K and Kumar, PV and Ramamohan, TR and Shivakumara, PV Dynamics and 'normal stress' evaluation of dilute suspensions of periodically forced prolate spheroids in a quiescent Newtonian fluid at low Reynolds numbers. Sadhana. ISSN 0256-2499 (In Press)

Madhukar, K and Ramamohan, TR and Shivakumara, IS The Effects of a Constant Bias Force on the Dynamics of a Periodically Forced Spherical Particle in a Newtonian Fluid at Low Reynolds Numbers. In: Numerical Analysis and Applied Mathematics. AIP , pp. 43-46.

Mahadevan, Srikrishna and Kapat, JS and Kumar, Rajan and Verma, SB (2016) Study of secondary flow and coolant film interaction in a high subsonic cascade. International Journal of Heat and Fluid Flow, 62. pp. 189-202. ISSN 0142727X

Mahajan, S and Kumar, A (1990) Solutions of two-dimensional euler equations with multigrid13; acceleration. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Majeed, M and Kar, IN (2015) Stochastic contraction-based observer and controller design algorithm with application to a flight vehicle. International Journal of Control, 88 (11). pp. 2291-2304. ISSN 00207179

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Majumdar, Sekhar and Rajani, BN and Kulkarni, DS and Mohan, Sripathi RANS Computation of Low Speed Turbulent Flow in Complex Configuration. In: State of the Art and Future Trends of CFD , 5 March, 2003, NAL, Bangalore.

Majumdar, Sekhar and Rajani, BN and Kulkarni, DS and Subrahmanya, MB CFD analysis of incompressible turbulent flow problems using unsteady RANS and large eddy simulation approach. In: International Conference in Ocean Engineering, ICOE 2009, 1-5 Feb 2009, Department of Ocean Engineering, IIT Madras, Chennai.

Majumdar, Sekhar and Rajani, BN and Kulkarni, DS and Subrahmanya, MB Unsteady RANS simulation of incompressible flow past a symmetric aerofoil at high angles of attack. In: Proceedings of the 12th Asian Congress of Fluid Mechanics, August 18-21, 2008, Daejeon, Korea.

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Natarajan, Kandasamy and Kumar, Rao Prakash and Reddy, PV and Nanje Gowda, NM and Rao, RMVGK (2000) Thermal and toughness property studies on a polybenzimidazole-modified epoxy resin system. Polymer International, 49. pp. 1321-1323.

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