Items where Author is "Rangarajan, R"

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Number of items: 22.

Conference or Workshop Item

Viswanathan, S and Narayana, CL and Ramesh, V and Desai, SS and Rangarajan, R (1993) Panel codes for aerodynamic analysis at NAL. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 9 July 1993, Sikkim, India.

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

Desai, SS and Rangarajan, R (1993) Development of full-potential codes in the decade 1983-1993. In: Proceedings of the Fluid Dynamics Symposium in Honour of Professor R. Narasimha on his 60th Birthday, 1993, Sikkim.

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.

Desai, SS and Rangarajan, R (1987) Viscous transonic flow over aerofoils using transonic full potential equation in a system of cartesion coordination AIAA-87-411. In: AIAA 25th aerospace science meeting, 12-15, Jan 1987, Reno, Nevada.

Journal Article

Singh, JP and Rangarajan, R and Ramaswamy, MA (1988) Computation of flow over airfoils under high lift separated flow condition 13; 13;. Journal of Aeronautical Society of India, 40 . pp. 105-110.

Proj.Doc/Technical Report

Singh, JP and Viswanathan, S and Rangarajan, R and Desai, SS (1996) Notes on the adaptation and validation of a panel code NALSOF0509 for the calculation of pressure distribution and overall coefficients on wings, bodies and wing-body-tail combinations in sub- and supersonic flows. Project Report. NAL, Bangalore.

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.

Singh, JP and Rangarajan, R and Desai, SS (1988) On the assessment of quot;Correctabilityquot; of data in two-dimensional transonic wind tunnel tests. Technical Report. National Aeronautical Laboratory, Bangalor, India.

Desai, SS and Rangarajan, R (1988) Mathematical modelling and computer simulation using cartesian grid. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desai, SS and Rangarajan, R (1986) Prediction of viscous effects on an aerofoil using transpiration model for the effects of boundary layer and wake. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desai, SS and Rangarajan, R (1986) Viscous transonic flow over aerofoils using transonic full potential equation in a system of cartesian coordinates. 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.

Singh, JP and Rangarajan, R and Ramaswamy, MA (1985) Computatian of flow over airfoils under high 11ft separated flow conditions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

Desai, SS and Narayana, CL and Rangarajan, R (1985) Extension to the Panel Code NALSOP0509 to Include Design of Wing-Body Configurations for Minimum Induced Drag at given lift and pitching moment. Project Report. National Aerospace Laboratories, Bangalore.

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.

Rangarajan, R and Ramaswamy, MR (1976) Design of 2nd DIA strain gauge balance with replaceable axial force unit. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rangarajan, R and Viswanathan, S (1970) Data reduction program for floating frame balances. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Seetharam, HC and Rangarajan, R (1970) Force calibration of AGARD B model in transonic flow mach numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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