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

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Ramesh, V (2002) Least squares grid free kinetic upwind method. PhD thesis, Indian Institute of Science, Bangalore.

A

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

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.

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

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

B

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

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

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

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

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

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

Bera, Rajendra K (1989) An Accurate method for calculating the initial development of vortex sheets. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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

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

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

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

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

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

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

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

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

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

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

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

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

C

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

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

Chakrabarthy, 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 (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, S (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 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, 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

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.

D

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.

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

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

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

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.

G

Girija, G and Basappa, - and Raol, JR and Padma, Madhuranatha (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 (1991) The role of residual nonturbulent disturbances on transition onset in two-dimensional boundary layers. Journal of Fluids Engineering, 113 . pp. 147-149.

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

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

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

H

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

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

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

J

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.

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

K

Kailas, Sudarsha V 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

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

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.

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

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 Pal, 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, Roddom 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.

M

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.

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

Majumdar, S 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 (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.

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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.

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

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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.

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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.

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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.

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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.

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T

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V

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

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

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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

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Y

Yajnik, K (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 (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 (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.

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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.

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