Up a level |

- NASA Aerospace Subject Categories (466)
- ENGINEERING (466)
**Fluid Mechanics and Thermodynamics**(466)

- ENGINEERING (466)

Group by: Creators | Item Type

Number of items at this level: **466**.

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

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
(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.

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

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

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.

Kidambi, R
(2006)
*Oscillatory Stokes flow in a cylindrical container.*
Fluid Dynamics Research, 38.
pp. 274-294.

Kidambi, R
(2003)
*Sloshing in Rotating Spherical Tanks Under Zero Gravity Conditions.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Kidambi, R. and Srinivasan, U.
(2018)
*Is the subharmonic threshold always lower than the fundamental one in plane Poiseuille flow.*
Physics of Fluids, 30 (1).
ISSN 10706631

Krishnamoorthy, V
(1982)
*Effect of turbulence on the heat transfer in a laminar and turbulent boundary layer over a gas turbine blade.*
In: American Society of Mechanical Engineers, International Gas Turbine, 18-22 Apr 1982, London, England.

Krishnamoorthy, V and Pai, BR and Sreenath, GS
(1991)
*Heat transfer study of a turbine blade cooling passage with ribs, pin fins and lateral ejection holes.*
In: International Symposium on Air Breathing Engines, 1-6 Sep 1991, Nottingham, England.

Krishnamoorthy, V and Pai, BR and Sukhatme, SP
(1988)
*Influence of upstream flow conditions on the heat transfer to nozzle guide vanes.*
Journal of Turbomachinery, Transactions, 110.
pp. 412-416.

Krishnan, V
(1986)
*Axisymmetric turbulent boundary layer on the cylindrical portion of an afterbody test model.*
In: 15th International Symposium on Space Technology and Science, 19-23 May 1986, Tokyo, Japan.

Krishnan, V
(1985)
*Axisymmetric turbulent boundary layer on the cylindrical portion of an afterday test model.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Krishnan, V
(1985)
*A method for determination of turbulent boundary layer skin friction from the measured velocity profile.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Krishnan, V and Yajnik, KS
(1989)
*Observations on turbulent boundary layer and the near wake of an afterbody.*
In: 10th Australasian Fluid Mechanics Conference, Dec 1989, Melbourne, Australia.

Krishnan, V and Yajnik, KS
(1988)
*A method for determination of turbulent skin friction when the coefficients of log-law may differ from universal constants.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Krishnan, VS and Ramamoorthy, P
(1993)
*VAYU CHAKRA - Wind Turbine Animation Software.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Kulkarni, DS and Mahendran, N and Majumdar, Sekhar
(2005)
*Laminar mixed convective heat transfer in a bottom heated lid
driven square cavity.*
Project Report.
National Aerospace Laboratories, Bangalore.

Kulkarni, DS and Majumdar, Sekhar
(2005)
*Navier stokes solution for two dimensional laminar convective heat transfer problems.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Kulkarni, DS and Rajani, BN and Majumdar, Sekhar
(2001)
*Studies on the Temporal and Spatial Discretisation Schemes Used in a Pressure Based RANS Algorithm For Incompressible Flow.*
Project Report.
National Aerospace Laboratories, Bangalore.

Kulkarni, DS and Sarkar, S and Majumdar, Sekhar
*Relative assessment of different turbulence models in prediction of airfoil characteristics for a wide range of angle of attack.*
In: International Conference on Theoretical, Applied, Computational and Experimental Mechanics, December 27-29, 2007, IIT Kharagpur.

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

Kumar, A and Yajnik, KS
(1980)
*Internal separated flows at large reynolds number.*
Journal of Fluid Mechanics, 97.
pp. 27-51.
ISSN 0022-1120

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.

Kumar, Anand
(1994)
*Burst Vortex Flow-field on a Delta Wing - A Numerical Simulation Using Euler Equations.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Kumar, Anand
(1985)
*Direct methods for solving elliptic equations.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Kumar, Anand
(1994)
*Effect of artificial viscosity on numerical simulation of leading-edge vortex breakdown.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Kumar, Anand
(1987)
*Euler solutions with a multi-block structured code.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Kumar, Anand
(1989)
*Flow calculation over a delta-wing using the thin-layer wavier-stokes equations.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Kumar, Anand
(1989)
*Flow-calculation over a delta-wing using the thin-layer Navier-Stokes equations.*
In: 3rd International Symposium on Computational Fluid Dynamics, 28-31 Aug 1989, Nagoya, Japan.

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.

Kumar, Anand and Das, A
(1987)
*Numerical solution of flow fields around delta wings using euler equations method.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Kumar, Anand and Dhanalakshmi, K
(1985)
*Algebraic grid generation for an airfoil.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

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.

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, 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.

Kumaresan, G and Kale, A
(2016)
*Application of L1 adaptive controller for the design of a novel decentralized leader follower formation algorithm.*
IFAC-PapersOnLine, 49 (1).
pp. 706-711.
ISSN 24058963

Lathasree, P and Pashilkar, AA and Sundararajan, N
(2019)
*Application of Generic Flight Controller Design Approach for A Delta Canard Fighter AircraftADMIRE.*
In: 6th Indian Control Conference, ICC 2019, 18-20 December 2019, Hyderabad, India.

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

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
(1994)
*Pressure based finite volume algorithm for viscous flow computation.*
In: CFD: Advances and Applications, 1994, India.

Majumdar, Sekhar
(1994)
*Turbulence modeling for CFD, part 1.*
In: CFD: Advances and Applications, 1994, India.

Majumdar, Sekhar
(1994)
*Turbulence modeling for CFD, part 2.*
In: CFD: Advances and Applications, 1994, India.

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.

Majumdar, Sekhar and Rodi, W and Zhu, J
(1990)
*Three-dimensional finite-volume method for incompressible flows with complex boundaries.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Majumdar, Sekhar and Vengadesan, S
(1992)
*Numerical computation of turbulent incompressible flow around aerofoils.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Manu, YC and Rajesh, A and Subrahmanya, MB and Kulkarni, DS and Rajani, BN
(2014)
*Simulations using transitional models with in the framework of RANS.*
In: IUTAM Symposium on Advances in Computation, Modeling and Control of Transitional and Turbulent Flows , 15 Dec 2014, Goa, India.

Mathew, Joseph and Basu, AJ
(1994)
*The mechanism of entrainment in circular jets.*
In: 14th International Conference on Numerical Methods in Fluid Dynamics, 11-15 Jul 1994, Bangalore, India.

Mathur, JS
(1992)
*Computation of inviscd flow over a two element airfoil using unstructured grids.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Mathur, JS
(1999)
*Grid generation for Aerospace applications.*
Journal of Aeronautical Society of India, 52 (3).
pp. 180-187.

Mathur, JS
(1993)
*Numerical grid generation.*
In: CFD: Advances and Applications, 1993, India.

Mathur, JS
(1991)
*Unstructured grid generation by delaunay triangulation: A User Manual.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Mathur, JS and Chakrabartty, SK
(1993)
*Grid generation package for high aspect ratio wings.*
In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 1993, Sikkim.

Mathur, JS and Chakrabartty, SK
(1992)
*An approximate factorisation scheme for elliptic grid generation with control functions.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Mathur, JS and Dhanalakshmi, K and Chakrabartty, SK
(1996)
*Euler Computations for the GSLV Using the JUEL3D Code.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Mathur, JS and Weatherill, NP
(1991)
*The numerical simulation of invisid compressible aeronautical flows.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Mathur, NB and Krishnan, V and Yajnik, KS
(1987)
*Base Flow Facility Progress Report for 1986-37.*
Project Report.
National Aerospace Laboratories, Bangalore.

Mathur, NB and Ramesh, G and Karunakaran, KM and Yajnik, KS
(1986)
*Continous colouhed smoke-wire technique for flow visulisation in wind tunnels.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Mathur, NB and Ramesh, G and Yajnik, KS
(1988)
*Continuous coloured smoke-wire technique for flow visualisation.*
Journal of Aeronautical Society of India, 40.
pp. 131-137.

Mathur, NB and Sreekanth, AK
(1988)
*Separated transonic interaction characterstics of an afterbody configuration in presence of a central propulsive jet.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Matsuzaki, R
(1975)
*Nonequilibrium flow of nitrogen behind a strong normal shock wave.*
Physical Society of Japan, 39.
pp. 1608-1613.

Menon, A and Choudhury, Balamati and Jha , RM
(2014)
*Adaptive Tuning in Terahertz Metamaterials using Swarm Intelligence.*
In: Metamaterial Symposim, ICCES14, 12 Jun 2014, South Korea.

Mohamed, Majeed
(2017)
*System identification of flexible aircraft in frequency domain.*
Aircraft Engineering and Aerospace Technology, 89 (6).
pp. 826-834.
ISSN 17488842

Mohamed, Majeed and Rong, S
(2021)
*Neural Partial Differentiation-Based Estimation of Terminal Airspace Sector Capacity.*
SAE International Journal of Aerospace, 14 (2).
p. 1.
ISSN 19463855

Mohamed, Majeed and Swaroop, S
(2016)
*Model simplification methods for a reduced order system of flexible aircraft.*
In: 2015 International Conference on Control Instrumentation Communication and Computational Technologies, 18-19 December 2015, Kumaracoil, India.

Mudkavi, Vidyadhar Y
(1994)
*Computation of vortex breakdown.*
In: CFD: Advances and Applications, 1994, India.

Mukund, R and Viswanath, PR and Narasimha, R and Prabhu, A and Crouch, JD
(2006)
*Relaminarization in highly favourable pressure gradients on a convex surface13;.*
Journal of Fluid Mechanics, 566 (--).
pp. 97-115.

Muralidhara, HS and Shembharkar, TR and Pai, BR and Ramanujam, PS and Jayaprakash, GN and Pandey, PK
(2001)
*Cold flow analysis of an aero-engine gas turbine combustor configuration 13; 13;.*
In: International Symposium on Air Breathing Engines, 3-7 Sept 2001, Bangalore, India.

Murthy, Krishna K
(1991)
*Graphic display of cockpit instruments for flight simulation.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Murugan, M
(1993)
*CIOPE - Console input/output operation on the processing elements.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Murugan, J N and Chutkey, Kiran and Verma, SB
(2019)
*Influence of base cavity on base pressure at subsonic and supersonic Mach numbers.*
In: AIP Conference Proceedings.

Muthuselvan, G and Muralidhara, HS and Kotegar, P and Gupta, S and Shankar, S and Deekshith, M and Mourya, S and Kumar, A
(2017)
*Computational analysis on primary breakup and deformation of kerosene jet in subsonic cross flow using VOF method.*
In: ASME 2017 Gas Turbine India Conference, GTINDIA 2017, 7 - 8 December 2017, Bangalore, India.

Nagarajan, Kaushik Kumar and Cordier, L and Airiau, C
(2013)
*Development and application of a reduced order model for the control of self-sustained instabilities in cavity flows.*
Communication in Computational Physics, 14.
pp. 186-218.
ISSN 1991-7120

Nagarajan, K.K. and Singha, S. and Cordier, L. and Airiau, C.
(2018)
*Open-loop control of cavity noise using Proper Orthogonal Decomposition reduced-order model.*
Computers and Fluids, 160.
pp. 1-13.
ISSN 00457930

Naidu, VPS
(2010)
*Fusion architecture for 3D target tracking using IRST and radar measurements.*
Journal of Aerospace Sciences and Technology, 62 (3).
pp. 183-195.
ISSN 0972-950X

Nair, Manoj T and Saxena, SK
(2003)
*Implementation and Testing of LUSSOR Implicit Time Stepping Method in a Multi-block Code.*
Technical Report.
National Aerospce Laboratories, Bangalore, India.

Nair, Manoj T and Saxena, SK
(2004)
*Upwind implicit residual smoothing for a multi-block upwind reynolds averaged navier-stokes solver.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Narasimha, R
(1989)
*Building bridges between dynamical chaos and open-flow turbulence.*
In: 10th Australasian Fluid Mechanics Conference, Dec 1989, Melbourne, Australia.

Narasimha, R
(1988)
*Introduction to irreducible tensor methods, Part 1.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Narasimha, R
(1990)
*Modelling the transitional boundary layer 13; 13;.*
Technical Report.
National Aeronautics and Space Administration, Virginia, USA.

Narasimha, R
(1986)
*Order and chaos in fluid flows.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Narasimha, R
(1991)
*Recent Advances in the Dynamics of the Transition Zone.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Narasimha, R
(1991)
*Recent advances in the dynamics of the transition zone.*
Technical Report.
National Aerospace Laboratories, Bangalore,India.

Narasimha, R
(1991)
*Recent advances in the dynamics of the transition zone.*
In: International Symposium on Air Breathing Engines, 1-6 Sep 1991, Nottingham, England.

Narasimha, R
(1985)
*Rockets in Mysore and Britain, 1750-1850 A.D.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

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
(1984)
*The prospects of turbulence management.*
In: 13th Fluid Mechanics and Fluid Power Conference, 12 Dec 1984, Thiruchirapalli, India.

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 Das, P
(1988)
*A spectral solution of the Boltzmann equation for the infinitely strong shock.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Narasimha, R and Dey, J
(1985)
*A note on certain recent intermittency data.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Narasimha, R and Kailas, SV and Kaimal, JC
(1990)
*Turbulent bursts in a near-neutral atmospheric boundary13; layer - part I.*
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.

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.

Nirmala, GA and Ramamoorthy, P
(1988)
*NCSU Code for the determination of airloads on a Light Aircraft Fuselage and its application to LCRA.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Nusrath, K and Singh, Jatinder and Basappa, B
(2016)
*Drag assessment of a high performance aircraft using system identification techniques.*
In: 2016 Indian Control Conference, ICC 2016 - Proceedings, 4-6 January 2016, Hyderabad, India.

Padma, Madhuranath
(2006)
*Bharathiya vayu yathayath ka anukaran Dwara vishleshan (Hindi version).*
Project Report.
National Aerospace Laboratories.

Pai, BR and Lakshminrayanan, R
(1981)
*Film cooling performance of liner cooling devices.*
In: International Symposium on Air Breathing Engines, 16-22 Feb 1981, Bangalore, India.

Pappu, VSR and Steck, JE and Guruganesh, R
(2016)
*Turbulence effects on modified state observer-based adaptive control: Black kite micro aerial vehicle.*
Aerospace, 3 (1).
pp. 1-22.
ISSN 22264310

Poornima, N and Senthil Kumaran, R and Jagannatha Rao, B and Swamy, KMM
(2009)
*Instrumentation and Data Acquisition System For Large Scale Rotating Rig.*
Technical Report.
National Aerospace Laboratories.

Prabhu, DK
(1993)
*High-temperature effects in hypersonic flows.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Prabhu, DK
(1995)
*Rotational-vibrational energies of diatomic hydrogen using the finite-element method.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Prabhu, DK
(1995)
*Vibrational energies of diatomic molecules using the finite-element method.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Prabhu, DK and Dwarakanath, GS and Suresh, BM
(1993)
*Approximation using rational splines with adjustable tension.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Prabhu, DK and Ravi, K
(1992)
*A note on the eigenvalues and eigenvectors for upwind methods.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Prabhu, DK and Subramanian, NR and Saxena, SK
(1993)
*Hypersonic viscous flow computations using parabolized navier-stokes equations.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Prabhu, Dinesh K
(1993)
*Computation of nonequilibrium flows using PNS equations 13; 13;.*
In: Symposium on Fluid Dynamics, 1993, Sikkim, India.

Pradeep, Shetty and Subrahmanya, MB and Kulkarni, DS and Rajani, BN
(2013)
*CFD Simulation of Flow Past Micro Air Vehicle Wings.*
Project Report.
National Aerospace Laboratories, Bangalore.

Pradeep, Shetty and Subrahmanya, MB and Kulkarni, DS and Rajani, BN
(2011)
*CFD simulation of flow past MAV wings.*
In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Prasad, S Ganesh and Ramamoorthy, P
(1990)
*Development of a shell program for the BGK code.*
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.

Puttam, JK
(2017)
*A combined implementation of overset grid and patched grid methodologies.*
Springer, New Delhi, pp. 477-486.
ISBN 978-81-322-2741-0

Rajani, BN and Kandasamy, A and Majumdar, Sekhar
(2012)
*On the reliability of eddy viscosity based turbulence
models in predicting turbulent flow past a circular cylinder
using URANS approach.*
Journal of Applied Fluid Mechanics, 5 (11).
pp. 67-79.
ISSN 17353572

Rajani, BN and Mittal, Naveen and Govindarajan, Rama
(1995)
*Linear stability analysis of the flow around natural laminar flow airfoils.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Rajani, BN and Subrahmanya, MB and Vinay Kumar , KN and Rajesh, A
(2013)
*Numerical Simulation of Flow Past a Prolate Spheroid.*
In: IIST Research Scholars Day- 2013, 16 Dec 2013, Thiruvananthapuram.

Rajani, BN and Viswanathan, S
(1995)
*Comparison of two candidate airfoils for LTA application.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Rajani, BN and Kandasamy, A and Majumdar, Sekhar
(2016)
*LES of flow past circular cylinder at Re = 3900.*
Journal of Applied Fluid Mechanics, 9 (3).
pp. 1421-1435.
ISSN 17353572

Rajappa, N and Leelavathi, K
(1986)
*On solving the nonlinear equations arising in the application of on-body kutta condition in Hess' panel method.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Rajappa, N and Leelavathi, K
(1987)
*Pressure distributions on an under-water store : I.*
Project Report.
National Aerospace Laboratories, Bangalore.

Rajeevalochanam, P and Ganesh Banda, BV
(2017)
*Mechanical Design and Analysis of Ceramic Stator Blades for Gas Turbine Stage.*
In: Materials Today: Proceedings.

Rajeevalochanam, P and Kumaran, RS and Sunkara, SNA and Kalita, N and Sharath, PP
(2017)
*Experimental and numerical studies on a curved back transonic airfoil.*
In: ASME 2017 Gas Turbine India Conference, GTINDIA 2017, 7 - 8 December 2017, 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.

Rajeevalochanam, P and Sunkara, S.N.A and Ramana Murthy, S.V and Kumaran, R.S
(2020)
*Design of a two spool contra-rotating turbine for a turbo-fan engine.*
Propulsion and Power Research, 9 (3).
p. 15.
ISSN 2212540X

Rajeevalochanam, P and Sunkara, SNA and Mayandi, B and Banda, BVG and Chappati, VSk and Kumar, K
(2016)
*Design of highly loaded turbine stage for small gas turbine engine.*
In: Proceedings of the ASME Turbo Expo, 13-17 June 2016, Seoul, South Korea.

Rajendran, S and Prathap, Gangan
(1999)
*Convergence of eigenvalues of a cantilever beam with 8- and 20-node hexahedral elements.*
Journal of Sound and vibration, 227 (3).
pp. 667-681.

Rajesh, A and Kulkarni, DS and Rajani, BN
(2013)
*Numerical Analysis of Transitional Flow Past Flat Plate.*
In: Fortieth National Conference on Fluid Mechanics and Fluid Power, 12-14 Dec 2013, National Institute of Technology (NIT), Hamirpur (HP).

Rajesh, A and Vinay Kumar , KN and Subrahmanya, MB and Kulkarni, DS and Rajani, BN
(2014)
*Flow past 6:1 prolate spheroid - A numerical study.*
In: 16th Annual CFD Symposium , 11-12 Aug 2014, CSIR-NAL, Bangalore.

Ramakrishnan, SV and Shankar, PN
(1982)
*The Oseen model for internal separated flows.*
Journal of Engineering Mathematics, 16.
pp. 325-347.
ISSN 0022-0833

Ramamohan, TR and Shivakumara, IS and Madhukar, K
(2009)
*Numerical simulation of the dynamics of a periodically forced spherical particle in a quiescent Newtonian fluid at low Reynolds numbers.*
In:
Lecture notes in Computer Science.
Lecture Notes in Computer Science, 5544
(5544/2).
Springer-Verlag, Heidelberg, Germany, pp. 591-600.
ISBN 978-3-642-01969-2

Ramamohan, TR and Shivakumara, IS and Madhukar, K
(2011)
*The dynamics and rheology of a dilute suspension
of periodically forced neutrally buoyant spherical
particles in a quiescent Newtonian fluid at low
Reynolds numbers.*
Fluid Dynamics Research, 43 (4).
045502.
ISSN 0169-5983

Ramamohan, TR and Srinivas, S and Subramanyam, A. Reddy
(2012)
*A study on thermal-diffusion and diffusion-thermo effects
in a two-dimensional viscous flow between slowly expanding
or contracting walls with weak permeability.*
International Journal of Heat and Mass Transfer, 55 (11-12).
pp. 3008-3020.
ISSN 0017-9310

Ramamoorthy, P
(1996)
*Derivation of NAL - OOXX airfoils from the Sunya airfoil.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ramamoorthy, P
(1988)
*A new method for designing natural laminar flow airfoils.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Ramamoorthy, P and Dhanalakshmi, K
(1987)
*NCSU Code: Validation and extension on NAL's UNIVAC 1100/60 system.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Ramamoorthy, P and Prasad, SK
(1989)
*Analysis and Design of Symmetrical Airfoils.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ramamoorthy, P and Premageetha, BK
(1991)
*'Aerowing' - The software for aerodynamic analysis of a large aspect-ratio finite wing at low speeds.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Ramamoorthy, P and Premageetha, BK
(1991)
*Application of 'Aerovvingquot; software for obtaining the viscous loads on the NALLA wing.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Ramamoorthy, P and Shankar, J
(1985)
*Subscritical pressure distributions on longez and varieze airfoils.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Ramesh, V
(2011)
*Unsteady meshfree solver - LSKUM-MN.*
In: Meshfree-2011 Conference, 10-11 Jan 2011, IISc, Bangalore.

Ramesh, V and Deshpande, SM
(2006)
*Unsteady computations for flow past two oscillating airfoils.*
In: 9th Proceedings of AeSI CFD Symposium, 11-12 Aug 2006, Bangalore, India.

Ramesh, V and Deshpande, SM
(2006)
*Unsteady flow computations for flow past multiple moving boundaries.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Rana, Davinder and Patel, Sandeep and Onkar, AK and Manjuprasad, M
(2011)
*Time domain simulation of airfoil flutter using fluid structure coupling through FEM based CFD solver.*
In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

Rangachari, Kidambi
(2011)
*Damping of surface waves in a brimful circular cylinder with a contaminated free surface.*
Fluid Dynamics Research, 43.
ISSN 0169-5983

Rangarajan, R
(1993)
*Computation of inviscid flows: Full potential method.*
In: CFD: Advances and Applications, 1993, Bangalore, India.

Rao, AV and Majumdar, Sekhar
(1992)
*A pressure based method for numerical computation of13; compressible flow.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Rao, DM
(1971)
*A method of flow stabilisation with high pressure recovery in short, conical diffusers.*
The Aeronautical Journal, 75.
pp. 336-339.

Rao, JR and Girija, G
(2000)
*Square-root information filter based sensor data fusion algorithm.*
In: Proceedings of IEEE International Conference on Industrial Technology, 19-22 Jan 2000, Bangalore, India.

Rao, KVL and Lefebvre, AH
(1976)
*Minimum ignition energies in flowing kerosene-air mixtures.*
Combustion and Flame, 27.
pp. 1-20.
ISSN 0010-2180

Rao, MNB
(1980)
*Solutions to heat-conduction problems by a mixed method.*
International Journal of Heat and Mass Transfer, 23.
pp. 443-450.
ISSN 0017-9310

Rao, MNB and Kumaran, KSS
(1974)
*Stress analysis of a compressor assembly subjected to mechanical and thermal loadings.*
In: Seminar on the Role of Computers in Structural Analysis, Design and Optimisation, 13-14 Jun 1974, Bangalore, India.

Rao, Sanjeev K
(2000)
*An Oseen-type model for swirling internal separated flows.*
Journal of Engineering Mathematics, 38 (2).
pp. 119-140.
ISSN 0022-0833

Rao, Sanjeev K
(1999)
*A model for flows with massive separation.*
Journal of Fluids Engineering, 121 (4).
pp. 917-919.
ISSN 0098-2202

Raol, JR and Sinha, NK
(1988)
*Estimation of states and parameters of stochastic nonlinear system with measurement corrupted by correlated noise13;.*
Problems of Control and Information Theory, 17 (3).
pp. 145-158.

Ravi, R and Deshpande, MD
(1986)
*Computation of plane jet impingement on a plate.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Ravichandran, KS
(1994)
*CUD-3 schemes with runge-kutta time stepping for euler equations.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ravichandran, KS
(1995)
*Explicit Third Order Compact Upwind Difference Schemes for13; Compressible Flow Calculations.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ravichandran, KS
(1994)
*Finite-volume upwind schemes for inviscid gas dynamics 13; 13;.*
In: CFD: Advances and Applications, 1994, India.

Ravichandran, KS
(1994)
*Flux-Vector Splitting Schemes for Euler Equations - A Ready Reference.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ravichandran, KS
(1992)
*High Resolution Schemes for Euler Equation in 2-D Plane Flow.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ravichandran, KS
(1994)
*Higher Order KFVS13; Schemes Using Compact Upwind Operators.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ravichandran, KS
(1994)
*Numerical Experiments on Shock Wave Diffraction Using Flux vector Splitting Schemes.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Ravichandran, KS and Kumar, Anand
(1991)
*Compact upwind algorithms for the scalar conservation law13; computational evaluation and comparisons for an initial value problem.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Revathi, A and Rao, Sandhya and Kavitha, Rao V and Singh, MM and Sendil, Murugan M and Srihari, Shylaja and Dayananda, GN
(2013)
*Effect of strain on the thermomechanical behavior of epoxy based shape memory polymers.*
Journal of Polymer Research, 20 (113).
pp. 1-10.
ISSN 1572-8935

Revathi, A and Sandhya, Rao and Kavitha, Rao V and Muralidhar, S and Sendil, Murugan M and Shylaja, Srihari and Dayananda, GN
(2013)
*Effect of strain on the thermomechanical behavior of epoxy based Shape memory polymers.*
Journal of Polymer Research, 20 (5).
pp. 1-10.
ISSN 1022-9760

Sajjan, Sharanappa V and Dutta, Vimala and Dutta, PK
(2008)
*Numerical simulation of flow over pitching bodies using an implicit reynolds averaged navier stokes solver.*
In: Proceedings of the 12th Asian Congress of Fluid Mechanics, 18-21 Aug 2008, Daejeon, Korea.

Sanjay, K
(1989)
*Parallel algorithm for Euler equations (one and two dimensional) using kinetic fiyx vector splitting.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sanjay, K and Sinha, UN and Shankar, PN
(1989)
*Laplace solver.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sarasamma, VR and Ramamoorthy, P
(1987)
*Computation of pressures on under-water-bodies.*
Project Report.
National Aerospace Laboratories, Bangalore.

Sathianarayanan, A and Venkatakrishnan, L and Sharma, SD
(2017)
*Control of low speed cavity flow using streamwise tabs at leading edge.*
In: AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, 9 - 13 January 2017, Grapevine, Texas.

Sathianarayanan, A and Verma, SB
(2017)
*Experimental investigation of an incident shock-induced interaction near an expansion corner.*
Journal of Spacecraft and Rockets, 54 (3).
pp. 769-773.
ISSN 00224650

Savanur, RA and Mudkavi, Vidyadhar Y
(2009)
*ANSYS modeling of the 500 kW Horizontal-axis wind turbine blade.*
Technical Report.
NAL.

Savanur, RA and Mudkavi, Vidyadhar Y
(2009)
*Aeroelastic study of horizontal-Axis wind turbine blade.*
Technical Report.
NAL.

Savanur, RA and Sharanappa, Sajjan V and Mudkavi, Vidyadhar Y
(2009)
*Three-dimensional CFD analysis of undeformed and deformed 500 kW horizontal-axis wind turbine blade.*
Technical Report.
NAL.

Saxena, SK
(1994)
*Hypersonic viscous flow computations.*
In: CFD: Advances and Applications, 1994, India.

Saxena, SK
(1992)
*An upwind formulation for the solution of thin-layer Navier-stokes equations.*
Journal of Aeronautical Society of India, 44 (3).
pp. 253-257.

Saxena, SK and Anamika, HS
(1993)
*Implicit step formulalion for compressible thin layer navier-stokes solution.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Saxena, SK and Dey, Debashis
(1993)
*High resolution TVD schemes for navier-stokes solution at13; supersonic/ hypersonic speeds.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Saxena, SK and Ravi, K
(1993)
*Some aspects of three dimensional supersonic/hypersonic 13; inviscid blunt body flow computations employing high resolution TVD schemes based on Roe's Riemann solver.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Selvarajan, S and Tulapurkara, EG and Ram, Vasanta V
(1998)
*A numerical study of flow through wavy-walled channels.*
International Journal for Numerical Methods in Fluids, 26.
pp. 519-531.

Sengupta, TK and Suman, VK and Bhumkar, YG
(2012)
*Control of bypass transitional flow past an aerofoil by plasma actuation.*
International Journal of Emerging Multidisciplinary Fluid Sciences, 3 (2-3).
pp. 117-134.
ISSN 1756-8315

Sengupta, TK and Suryanarayana, GK and Selvarajan, S
(1987)
*A case for turbulence management by imposed wall excitation for fully developed turbulent flows - A numerical study.*
In: IUTAM Symposium on Turbulence management and relaminarisation, 13-23 Jan 1987, Bangalore, India.

Sengupta, A and Sengupta, T.K. and Sengupta, S. and Mudkavi, V.
(2018)
*Effects of error on the onset and evolution of Rayleigh–Taylor instability.*
Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 135.
pp. 233-239.
ISSN 16122909

Sengupta, S and Sengupta, TK and Puttam, JK and Vajjala, KS
(2020)
*Global spectral analysis for convection-diffusion-reaction equation in one and two-dimensions:
Effects of numerical anti-diffusion and dispersion.*
Journal of Computational Physics, 408.
ISSN 00219991

Senthil Kumaran, R and Swamy, KMM
(2007)
*CASCADE TESTS ON CE 20 LOX TURBINE NOZZLE BLADE PROFILE.*
Technical Report.
National Aerospace Laboratories.

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 and Narayan, KY
(1987)
*Shock-induced separated flows on the lee surface of delta wings.*
Aeronautical Journal, 91.
pp. 128-141.

Shankar, PN
(2005)
*Axial eigenfunctions and inhomogeneous solutions for the three-dimensional Stokes system with an application to natural convection in a cylinder13;.*
Zeitschrift fur Angewandte Mathematik und Physik, 56 (2).
pp. 254-272.
ISSN 0044-2275

Shankar, PN
(1991)
*Exact solutions for a class of nonlinear free surface flows.*
Proceedings: Mathematical and Physical Sciences, 434 (1892).
pp. 677-682.

Shankar, PN
(1988)
*Liquid-Vapour Phase change between plane liquid surfaces: A continuum analysis to determine real gas effects.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Shankar, PN
(1995)
*Low Reynolds number piston generated toroidal vortices.*
In: 6th Asian Congress of Fluid Mechanics, 22-26 May 1995, Singapore.

Shankar, PN
(2005)
*Moffatt eddies in the cone.*
Journal of Fluid Mechanics, 539.
pp. 113-135.
ISSN 0022-1120

Shankar, PN
(1991)
*On a Lemma of Lighthill's in Aerofoil Theory.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Shankar, PN
(1992)
*The Roots of sin Z = } Z.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Shankar, PN
(1992)
*Stokes Flow in the Driven Cavity.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Shankar, PN
(1998)
*Three-dimensional Stokes flow in a cylindrical container13;.*
Physics of Fluids, 10 (3).
pp. 540-549.
ISSN 1070-6631

Shankar, PN
(1997)
*Three-dimensional eddy structure in a cylindrical container.*
Journal of Fluid Mechanics, 342.
pp. 97-118.

Shankar, PN
(1993)
*The eddy structure in Stokes flow in a cavity.*
Journal of Fluid Mechanics, 250.
pp. 371-383.

Shankar, PN
(1992)
*A mapping relevant to the flow over a circular hump or ditch.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Shankar, PN
(2005)
*A new separation of variables method for complex geometries.*
Current Science, 88 (2).
pp. 266-269.
ISSN 0011-3891

Shankar, PN
(1979)
*A note on the growth of disturbances at an inviscid interface.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Shankar, PN
(2003)
*A simple method for studying low-gravity sloshing frequencies.*
Proceedings of the Royal Society of London, Series A: Mathematical, Physical and Engineering Sciences, 459 (2040).
pp. 3109-3130.
ISSN 1364-5021

Shankar, PN and Deshpande, MD
(1988)
*Experiments on liquid-vapour phase change between plane liquid surfaces Part I: experiments with water, freon and mercury.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Shankar, PN and Deshpande, MD
(1988)
*Experirnents on liquid-vapour phase change between plane liquid surfaces part 2: Observations of large temperature jumps near the Interfaces.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Shankar, PN and Deshpande, MD
(2000)
*Fluid mechanics in the driven cavity.*
Annual Review of Fluid Mechanics, 32.
pp. 93-136.

Shankar, PN and Deshpande, MD
(1990)
*Viscous and nonlinear effects in the gas dynamics of phase change.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Shankar, PN and Deshpande, MD and Radhakrishna, M
(1996)
*Experiments in Driven Cavity Flows.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Shankar, PN and Kidambi, R and Hariharan, J
(2003)
*Oscillatory eddy structure in a container.*
Journal of Fluid Mechanics, 494.
pp. 163-185.

Shankar, PN and Kumar, Manoj
(1994)
*Drop Generated Vortex Rings.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Shankar, PN and Sinha, UN
(1976)
*The Rayleigh problem for a wavy wall (impulsive motion generation of viscous fluid flow).*
Journal of Fluid Mechanics, 77.
pp. 243-256.
ISSN 0022-1120

Shankar, PN and Sinha, UN
(1980)
*Weakly sheared, two-dimensional inviscid flows past bodies.*
Journal de Mecanique, 19 (1).
pp. 125-148.

Shantha Kumar, N and Kashyap, SK
(2006)
*Target tracking an non-gaussian environment.*
Technical Report.
National Aerospace Laboratories, 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

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.

Shekhar, Shashi N
(1992)
*Perspective visualisation of aircraft flight.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Shikhar Jaiswal, A
(2017)
*Shape parameterization of airfoil shapes using Bezier curves.*
Lecture Notes in Mechanical Engineering, PartF9.
pp. 79-85.
ISSN 21954356

Shubha, G
(1995)
*MIS -Menu Initialisation Software.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Singh, GK and Claassens, J
(2010)
*An analytical solution for the inverse kinematics of a redundant 7DoF Manipulator with link offsets.*
In: International Conference on Intelligent Robots and Systems (IROS) 2010 IEEE/RSJ , 18-22 Oct. 2010, Taipei, Taiwan .

Singh, JP
(1993)
*Applications of multigrid methods to problems in CFD.*
In: CFD: Advances and Applications, 1993, India.

Singh, JP
(1989)
*Computation of viscous axisymmetric transonic flow using cartesian grids.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Singh, JP
(1989)
*Solution of laplace equation using full approximation storage multigrid technique.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Singh, JP
(2001)
*An improved Navier-Stokes flow computation of AGARD case-10 flow over RAE2822 airfoil using Baldwin-Lomax model.*
Acta Mechanica, 151 (3-4).
pp. 255-263.
ISSN 0001-5970

Singh, JP and Rangarajan, R and Ramaswamy, MA
(1985)
*Computatian of flow over airfoils under high 1ift separated flow conditions.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Singh, Manish K and Dhanalakshmi, K and Mathur, JS
(2011)
*Investigation of two dimensional flow past multi element airfoils for general transport aircraft.*
International Journal of Numerical Methods for Heat & Fluid Flow, 21 (8).
1026 -1049.
ISSN 0961-5539

Singh, Manish K and Ramesh, V and Balakrishanan, N
(2015)
*Implicit scheme for meshless compressible Euler solver.*
Engineering Applications of Computational Fluid Mechanics, 9 (1).
pp. 382-398.
ISSN 1994-2060 (Print), 1997-003X (Online)

Singh, PK and Mathur, JS
(1993)
*An initiative to 3-D multiblock elliptic grid generation.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Singha, Sintu and Sinhamahapatra, KP
(2011)
*Control of vortex shedding from a circular cylinder using imposed transverse magnetic field.*
International Journal of Numerical Methods for Heat & Fluid Flow, 21 (1).
pp. 32-45.
ISSN 0961-5539

Singha, Sintu and Nagarajan, Kaushik Kumar and Sinhamahapatra, KP
(2016)
*Numerical study of two-dimensional flow around two side-by-side circular cylinders at low Reynolds numbers.*
Physics of Fluids, 28 (5).
pp. 1-21.
ISSN 10706631

Sinha, Manish and Majumdar, Sekhar
(1993)
*Parallelisation of a navier-stokes code for three dimensional incompressible flows.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Sinha, UN
(1995)
*CFD on Flosolver.*
In: 6th Asian Congress of Fluid Mechanics, 22-26 May 1995, Singapore.

Sinha, UN
(1989)
*Outline of the method of complex characteristics.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Deshpande, MD and Sarasamma, VR
(1988)
*Flosolver: A parallel computer for fluid dynamics.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Sarasamma, VR
(1984)
*Calculation of axisymmetric transonic small perturbation equation using conservative scheme.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Sarasamma, VR
(1985)
*On boundary condition for transonic small perturbation equation for body having blunt leading edge.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Shankar, PN
(1989)
*A Fast Poisson Solver in Two Dimensions.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Sinha, UN and Shankar, PN
(1985)
*A fast solver in one dimension.*
Technical Report.
National Aeronautical Laboratory, Bangalore, 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
(2012)
*Numerical Computation of Unsteady Compressible Flow past
a Plunging Aerofoil.*
Journal of Applied Fluid Mechanics, 5 (4).
pp. 131-138.
ISSN 1735-3572

Sivaramakrishnan, K and Yajnik, KS and Jayaraman, V
(1988)
*Wind loads on sparse meshes used in antennae of large telescopes.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sivaramakrishnan, Rajalakshmy and Sarasamma, VR
(1992)
*Processing element selector for Flosolver Mk3.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Srikanth, VC and Majumdar, Sekhar
(1992)
*Relative performance of different low reynolds number turbulence models for prediction of fully developed channel13; flow.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Srikanth, A and Krishnamurthy, L and Prathyusha, L P and Naidu, VPS
(2016)
*Synthetic aerial image generation for miniature aerial system.*
In: International Conference on Trends in Automation, Communication and Computing Technologies, I-TACT 2015, 21-22 December 2015, Bangalore.

Srilatha, KR and Dwarakanath, GS and Ramamoorthy, P
(1989)
*Design of NAL-NLF-208-MARK 2 airfoil for NAL's light aircraft.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Srilatha, KR and Ramamoorthy, P
(1988)
*Allen's code for airfoil analysis.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Srinivas, K and Gururaja, J
(1979)
*An improved form of the artificial diffusion parameter-X.*
Journal of Computational Physics, 31.
pp. 289-292.
ISSN 0021-9991

Srinivas Rao, K and Subrahmanya, MB and Kulkarni, DS and Rajani, BN
(2009)
*Numerical Simulation of Turbulent flow past Micro Air Vehicle Wing sections.*
Project Report.
National Aerospace Laboratories, Bangalore.

Srinivasa, C
(1992)
*Multigrid Technique for Solving the Full Potential Equation on an Airfoil in Cartesian Grid.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Srinivasan, Radhakrishnan
(1994)
* Exact solutions of Rayleigh's equation and sufficient conditions for inviscid instability of parallel, bounded shear flows 13; 13;.*
Zeitschrift fuer angewandte Mathematik und Physik, 45 (4).
pp. 615-637.
ISSN 0044-2275

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.

Srivastava, A
(1991)
*Quadrilateral Vortex Panel Code Numerical Testing.*
Technical Report.
National Aerospace Laboratories, 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
(1994)
*Geometry Development of Complex Configurations.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Srivastava, Ashok
(1989)
*Prediction of aerodynamic characteristics of wing body combinations at high angles of attack experience with an13; existing code.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Srivastava, Ashok
(1993)
*A numerical procedure for efficient computations near sharp trailing edges of three dimensional wings.*
Technical Report.
National Aerospace Laboratories, 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
(1995)
*Note on the redundancy in the discrete-vortex method for closed bodies 13; 13;.*
In: Proceedings of the 4th Pan-American Congress of Applied Mechanics, 3-6 Jan 1995, Buenos Aires, Argentina.

Subrahmanya, MB and Kulkarni, DS and Rajani, BN
*Numerical simulation of low aspect ratio fixed wings for MAV applications.*
In: 8th Asian Computational Fluid Dynamics Conference, 10-14 January, 2010, Hong Kong.

Subrahmanya, MB and Rajani, BN and Kulkarni, DS and Rajesh, A
(2015)
*Transitional flow past low Re aerofoil.*
In: 17th Annual CFD Symposium, CFD Division, AeSI, 11-08-2015, NAL, Bangalore.

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 Chakrabartty, SK
(1985)
*Transonic flow computations around finite wings.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Chakrabartty, SK
(1986)
*Transonic potential flow computations around finite wings.*
Journal of Aeronautical Society of India, 38.
pp. 55-57.

Subramanian, NR and Dwarakanath, GS
(1966)
*Hypersonic flow around a blunt body - real gas effects.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Subramanian, NR and Kumar, Anand
(1989)
*Role of Supercomputer in Computational Aerodynamics.*
Technical Report.
National aerospace Laboratories, Bangalore,India.

Sudesh, K Kashyap and Naidu, VPS and Jatinder, Singh and Girija, G and Raol, JR
(2006)
*Tracking of multiple targets using interactive multiple model and data association filter.*
Journal of Aerospace Science and Technologies, 58 (1).
pp. 66-74.

Sudhakar, S and Chandankumar, A and Venkatakrishnan, L
(2017)
*Influence of propeller slipstream on vortex flow field over a typical micro air vehicle.*
Aeronautical Journal, 121 (1235).
pp. 95-113.
ISSN 00019240

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.

Sundaram, S
(1987)
*Observations on the hydrodynamic flow visualisation at O.N.E.R.A.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Sunil, S and Abhilash, JK and Kumar, A and Shukla, HK
(2019)
*Oxidative stabilization studies on pretreated polyacrylonitrile precursor fiber suitable for
carbon fiber production.*
In: AIP Conference Proceedings 2166.

Suresh, S and Naidu, VPS
(2019)
*Vibration Analysis of Heterogeneous Gearbox Faults using EMD Features and SVM Classifier.*
In: IOP Conference Series: Materials Science and Engineering.

Suryanarayana, GK and Meier, GEA
(1995)
*Effect of ventilation on the flowfield around a sphere.*
Experiments in Fluids, 19 (2).
pp. 78-88.
ISSN 0723-4864

Suryanarayana, GK and Pauer, Henning and Meier, GEA
(1993)
*Bluff-body drag reduction by passive ventilation.*
Experiments in Fluids, 16.
pp. 73-81.

Suryanarayana, GK and Prabhu, A
(2000)
*Effect of natural ventilation on the boundary layer separation and near-wake vortex shedding characteristics of a sphere.*
Experiments in Fluids, 29 (6).
pp. 582-591.

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, Kiran and Sivaramakrishnan, Rajalakshmy
(1990)
*Handling large disk I/O Operations on the Flosolver13;.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Syed, Z and Rajesh, A and Subrahmanya, MB and Rajani, BN
(2014)
*OpenFOAM Simulations for MAV Applications.*
In: 16th Annual CFD Symposium, 11-12 Aug 2014, CSIR-NAL, Bangalore.

Thomas, S and Choudhury, Balamati
(2016)
*Analysis of metamaterial cloaks using circular split ring resonator structures.*
Computers, Materials and Continua, 52 (3).
pp. 132-140.
ISSN 15462218

Tirumalesa, D
(1966)
*Discontinuous solutions in supersonic reacting gas flows (Discontinuous solutions in supersonic reacting gas flows under nonequilibrium conditions).*
Zeitschrift Fuer Angewandte Mathematik und Physik, 17.
pp. 707-717.

Tolstykh, AI and Ravichandran, KS
(1991)
*Compact upwind difference schemes for scalar conservation laws.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Tribhuvanam, S and Nagaraja, HC and Naidu, VPS
(2019)
*Arrhythmia classification with single beat ECG evaluation and support vector machine.*
International Journal of Innovative Technology and Exploring Engineering, 8 (12).
pp. 1-7.
ISSN 22783075

Ugargol, R and Narayanaswamy, KS and Sesha Kumar, CV
(2017)
*Life estimation of turbine blisk for a gas turbine engine.*
International Journal of Mechanical Engineering and Technology, 8 (8).
pp. 393-399.
ISSN 09766340

Vajjala, KS and Sengupta, TK and Mathur, JS
(2020)
*Effects of numerical anti-diffusion in closed unsteady flows governed by two-dimensional NavierStokes equation.*
Computers and Fluids, 201.
ISSN 00457930

Varadhan, Sundara G and Sinha, UN
(1989)
*Serial transfer between two nodes using synchronous mode.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Varute, PT
(1973)
*Hydraulic oil contamination studies at NAL.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Vasantha, R
(1994)
*Rolled-up wake field behind aircraft configurations.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Venkatakrishnan, L
(2005)
*Density measurements in an axisymmetric underexpanded jet by background-oriented schlieren technique.*
AIAA Journal, 43 (7).
pp. 1574-1579.
ISSN 0001-1452

Venkatakrishnan, L and Elavarasan, R and Bhat, GS and Krothapalli, A and Lourenco, L
(2003)
*Particle image velocimetry study of a cloud-like flow.*
Current Science, 85 (6).
pp. 778-785.
ISSN 0011-3905

Venkatesh, T and Pradeep, Shetty and Kulkarni, DS and Rajani, BN
(2012)
*CFD simulation using FLUENT and RANS3D - A validation exercise.*
Project Report.
National Aerospace Laboratories, Bangalore.

Venkatesh, TN
(2010)
*A numerical study of the role of vertical structure of vorticity during tropical cyclone genesis.*
Fluid Dynamics Research, 42 (045506).
ISSN 0169-5983

Venkatesh, TN and Sarasamma, VR and Rajalakshmy, S and Sahu, Kirti Chandra and Govindarajan, Rama
(2005)
*Super-linear speed-up of a parallel multigrid Navier-Stokes solver on Flosolver.*
Current Science, 88 (4).
pp. 589-593.

Verma, SB and Chidambaranathan, M and Hadjadj, A
(2018)
*Analysis of shock unsteadiness in a supersonic over-expanded planar nozzle.*
European Journal of Mechanics, B/Fluids, 68.
pp. 55-65.
ISSN 09977546

Verma, SB and Hadjadj, A
(2015)
*Supersonic flow control.*
Shock Waves, 25 (5).
pp. 443-449.
ISSN 09381287

Verma, SB and Manisankar, C
(2017)
*Assessment of various low-profile mechanical vortex generators in controlling a shock-induced separation.*
AIAA Journal, 55 (7).
pp. 2228-2240.
ISSN 00011452

Vimala, CS and Nath, G
(1975)
*Mass transfer effectiveness on three-dimensional laminar compressible boundary layer flows.*
Journal of Fluids Engineering, 97.
pp. 382-384.

Vinay, CA and Chakravarthy, B
(2017)
*Aerothermal analysis of insulation to protect exhaust ducts of a pusher turbo prop engine aircraft.*
Lecture Notes in Mechanical Engineering, PartF8.
pp. 843-851.
ISSN 21954356

Viswanath, PR and Ramesh, G and Madhavan, KT
(2000)
*Separation control by tangential blowing inside the bubble.*
Experiments in Fluids, 29 (1).
pp. 96-102.

Viswanathan, KS and Dwarakanath, GS and Shanbhag, VV
(1971)
*The structure of strong shock waves using the Fokker-Planck model (Shock wave structure in monatomic gases, using Fokker-Planck model for particle collisions and Mott-Smith distribution for shock front).*
Indian Academy of Sciences, Proceedings, 74 (Sec.A).
pp. 115-132.

Yajnik, KS
(1974)
*General integral properties of mixing layers.*
Journal of Mathematical and Physical Sciences, 8 (4).
pp. 327-340.

Yajnik, KS
(1973)
*General integral properties of mixing layers.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS
(1984)
*Impact of developments in electrical sciences on certain engineering disciplines and implications on engineering education.*
Technical Report.
National Aeronautical Laboratory, Bangalore,India.

Yajnik, KS
(1984)
*Integral transforms and boundary layers.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS
(1988)
*Limits and models in fluid mechanics 13; 13;.*
Developments in fluid mechanics and space technology (A89-50001 22-34).
pp. 299-312.

Yajnik, KS
(1987)
*The World of Chaos.*
Technical Report.
National Aerospace Laboratories, Bangalore, India.

Yajnik, KS and Deshpande, MD and Siddalingappa, SR
(1985)
*Experimental techniques for aerodynamic studies of high lift systems: Progress report 1984-85.*
Technical Report.
National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS and Gupta, Ramesh P
(1976)
*Strong interaction effects on upstream wall pressure in a separated flow with a forward-facing wall jet.*
In: AIAA 1976, 4-16 July 1976, United States.

Yajnik, KS and Sundaram, S and Acharya, M
(1983)
*Observations on large scale motions in highly disturbed boundary Layers.*
In: Structure of complex turbulent shear flow; Proceedings of the, 31 Aug - 03 Sept 1983, France.

Yajnik, KS and Sundaram, S and Sivaram, R
(1988)
*Evaluation of drag reduction by turbulence control devices 13; 13;.*
In: IUTAM Symposium on turbulence management and relaminarisation, 13-23 Jan 1987, Bangalore, India.