Items where Author is "Ravichandran, KS"

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Number of items: 26.

Conference or Workshop Item

Ravichandran, KS (1996) Flux split, higher order compact upwind difference schemes. In: Proceedings of the 3rd International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, 1-6 sept 1996, Beijing, China.

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

Ravichandran, KS (1993) Difference schemes for hyperbolic system of Conservation Laws 13; 13;. In: CFD: Advances and Applications, 1993, Bangalore, India.

Ravichandran, KS (1993) Introduction to multigrid methods. In: CFD: Advances and Applications, 1993, India.

Desai, SS and Rangarajan, R and Singh, JP and Ravichandran, KS (1987) Full potential flow computations using cartesian grids. In: AIAA 8th Computational Fluid Dynamics Conference.

Desai, SS and Rangarajan, R and Singh, JP and Ravichandran, KS (1987) Full-potential flow computations using cartesian grids 13; 13;. In: 8th Conference on Computational Fluid Dynamics, 9-11 June 1987, Honolulu, United States.

Journal Article

Srivastava, Ashok and Ravichandran, KS (2000) Novel Beetle algorithm for Cartesian grid generation in two13; dimensions. Journal of Aircraft, 37 (5). pp. 927-929. ISSN 0021-8669

Ravichandran, KS (1997) Higher Order KFVS Algorithms Using Compact Upwind13; Difference Operators. Journal of computational physics, 130 . pp. 161-173.

Ravichandran, KS (1992) Numerical experiments in I-D euler equations using higher order schemes. Journal of Aeronautical Society of India, 44 (3). pp. 233-243.

Desai, SS and Ragarajan, R and Singh, JP and Ravichandran, KS (1988) Full-potential calculations using Cartesian grids. Aeronautical Society of India, Journal, Vol. 4 . pp. 97-103.

Proj.Doc/Technical Report

Ravichandran, KS and Singh, JP (2000) A Computational Study of Two-species Spherical Explosion in Air. Project Report. National Aerospace Laboratories, Bangalore, India.

Srivastava, Ashok and Ravichandran, KS (1999) Cartesian Grid Vizualization Code (C ). Technical Report. National Aerospace Laboratories, Bangalore, India.

Srivastava, Ashok and Ravichandran, KS (1999) Cartesian Grid Generator (2-D). 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) Flux-Vector Splitting Schemes for Euler Equations - A Ready Reference. 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 (1994) CUD-3 schemes with runge-kutta time stepping for euler equations. 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 (1992) A non-oscillatory dissipation model for 1-D euler computations at high mach numbers. Technical Report. National Aeronautical Laboratory, 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.

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

Ravichandran, KS and Rangarajan, R and Desai, SS and George, KP (1988) Vortex simulation in full potential solver on a cartesian grid. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Ravichandran, KS and Desai, SS and Rangarajan, R (1986) Modification to the cartesian grid in 3-D potential code for flow past swept wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ravichandran, KS and Desai, SS and Rangarajan, R (1986) Modification to the cartesian grid in 3-D potential code for flow past swept wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desai, SS and Rangarajan, R and Ravichandran, KS (1985) A preliminary note on the development of a three-dimensional potential code in cartesian coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Thu Oct 30 02:01:41 2014 IST.