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**Fluid Mechanics and Thermodynamics**(440)

- ENGINEERING (440)

Group by: Creators | Item Type

Number of items at this level: **440**.

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

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

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.

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 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

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

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.

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.

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.

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.

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

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.

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

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.
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