Items where Author is "Viswanathan, S"

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.