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Number of items: 15.

Chakrabartty, SK (2005) Role Of Computational Fluid Dynamics In The Design Of Aerospace Configurations. Journal of Aerospace Sciences amp; Technology, 57 (1). pp. 24-32. ISSN 0971-950X

Deshpande, MD and Srinidhi, BG (2005) Bifurcation, period dubling and hysteresis in mixed convection in a cavity. Technical Report. National Aerospace Laboratories, Bangalore, India.

Deshpande, MD and Srinidhi, BG (2005) Flow in the driven cubical cavity: Generation of data for low Reynolds numbers. Technical Report. National Aerospace Laboratories, Bangalore, India.

Deshpande, MD and Srinidhi, BG (2005) Mixed convection in a generation of periodic and unsteady13; convection.13;. Technical Report. National Aerospace Laboratories, Bangalore, India.

Kidambi, R and Shankar, PN (2005) The effects of the contact angle on sloshing in containers. Proceedings of the Royal Society of London, 460 (2048). pp. 2251-2267. ISSN 1364-5021

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, KD and Mahendran, N and Majumdar, Sekhar (2005) Laminar mixed convective heat and transfer in a bottom heated ltd driven square cavity. Technical Report. National Aerospace Laboratories, Bangalore, India.

Nair, Manoj T (2005) Development of a two-dimensional Aerodynamic optimisation code based on sensitivity analysis. Technical Report. National Aerospace Laboratories, Bangalore, India.

Nair, Manoj T and Kumar, Naresh and Saxena, SK (2005) Computational Analysis of Inlet Aerodynamics for a Hypersonic Research Vehicle. Journal of Propulsion and Power, 21 (21). pp. 286-291.

Rajani, BN and Lanka, Harsha Gopal and Majumdar, Sekhar (2005) Laminar flow past a circular cylinder at reynolds number varying from 50 to 5000. Technical Report. National Aerospace Laboratories, Bangalore, India.

Saxena, S and Nair, M (2005) An Improved Roe Scheme for Real Gas Flows. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January 2005, Reno, Nevada.

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

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

This list was generated on Sat Oct 25 01:25:51 2014 IST.