Items where Author is "Viswanathan, S"

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Number of items: 13.

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.

Journal Article

Desai, SS and Viswanathan, S and Ramaswamy, MA (1977) Numerical evaluation of transonic wave drag. Journal of Aircraft, 14 (2). pp. 215-217. ISSN 0021-8669

Ramaswamy, MA and Viswanathan, S (1975) Some observations on the Adams body of minimum wave drag. Journal of Aircraft, 12 . pp. 1001-1002. ISSN 0021-8669

Proj.Doc/Technical Report

Mukherjee, Somenath and Prakash, B M Shashi and Alok, P Burgul and Viswanathan, S (2007) A method for dynamic characterization and response predication using ground vibration test(GVT) data for unknown structure. Technical Report. National Aerospace Laboratories, Bangalore, India.

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.

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

Viswanathan, S (1991) Application of a panel code for in house aircraft projects: Part I. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gopinath, R and Viswanathan, S and Desai, SS (1991) Preliminary Results on the Influence of Tunnel Wall Boundary Conditions on 2-D Transonic Full Potential Code. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sridharan, R and Viswanathan, S (1985) A Computer Code for Generating Plots of Load Distribution on Spanwise Sections on a wing. Project Report. National Aerospace Laboratories, Bangalore.

Desai, SS and Viswanathan, S (1980) Design of Axisymmatrec supersonic/hypersonic nozzles. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desai, SS and Viswanathan, S (1980) Design of axisymmetric supersonic/hypersonic nozzles. 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.

Viswanathan, S (1970) Programs to analyze supersonic flow past right circular cones with a view to make use of uncalibrated cones for determination of flow angles and mach numbers in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Wed Apr 23 18:22:56 2014 IST.