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Number of items: 24.

Conference or Workshop Item

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.

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

Saxena, SK and Ravi, K (1995) Computation of three dimensional supersonic and hypersonic blunt body flows using high resolution TVD schemes based on Roe's approximate Riemann Solver. In: 14th International Conference on Numerical Methods in Fluid Dynamics, 11-15 July 1994, Bangalore, India.

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

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.

Journal Article

Basu, AJ and Narasimha, R and Prabhu, A (1995) Modelling plane mixing layers using vortex points and sheets. Applied Mathematical Modelling, 19 (2). pp. 66-75.

Chakrabartty, SK and Dhanalakshmi, K (1995) Computation of transonic flows with shock-induced separation using algebraic turbulence models. AIAA Journal, 33 (10). pp. 1979-1981.

Kumar, M and Arakeri, JH and Shankar, PN (1995) Translational velocity oscillations of piston generated vortex rings. Physics of Fluids, 7 (11). pp. 2751-2756.

Saxena, SK and Ravi, K (1995) Computation of three dimensional supersonic and hypersonic blunt body flows using high resolution TVD schemes based on Roe's Approximate Riemann Solver. Lecture Notes in Physics (453). pp. 520-524.

Saxena, SK and Ravi, K (1995) Some aspects of high-speed blunt body flow computations with Roe scheme. AIAA Journal, 33 (6). pp. 1025-1031.

Shankar, PN and Kumar, M (1995) Vortex rings generated by drops just coalescing with a pool. Physics of Fluids, 7 (4). pp. 737-746. ISSN 1070-6631

Proj.Doc/Technical Report

Chakrabartty, SK and Dhanalakshmi, K and Mathur, JS (1995) Computation of Three-Dimensional Transonic Viscous Flow using the JUMBO3D Code. Technical Report. National Aerospace Laboratories, 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.

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.

Premalatha, (1995) C++ programming conventions. Technical Report. National Aerospace Laboratories, Bangalore, India.

Premalatha, (1995) Object Oriented Programming and C++. Technical Report. National Aerospace Laboratories, Bangalore, India.

Premalatha, and Ramamoorthy, P (1995) Small aircraft information system. Technical Report. National Aerospace Laboratories, Bangalore, India.

Premalatha, . (1995) A Brief Introduction to C. Technical Report. National Aerospace Laboratories, Bangalore, India.

Premalatha, . and Vidyadhar, Mudkavi (1995) An Implementation of linked Lists Using C++. Technical Report. National Aerospace Laboratories, Bangalore, India.

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

Rajani, BN and Mittal, Naveen and Govindrajan, Rama (1995) Linear stability analysis of the flow around natural laminar flow airfoils. 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.

Srivastava, Ashok and Mook, Dean T (1995) An Improved Vortex Method for Closed Surfaces. Technical Report. National Aerospace Laboratories, Bangalore, India.

This list was generated on Sat Aug 2 01:25:47 2014 IST.