Author:
Venkatapathy E,Tokarcik-Polsky S,Deiwert G
Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. Numerical simulation of unsteady flow in a hypersonic shock tunnel facility
2. Tokarcik-Polsky, S., Papadopoulos, P., Venkatapathy, E. and Deiwert, G. S. "The NASA Ames 16-Inch Shock Tunnel Nozzle Simulations and ExperimentalComparison," AIAA95-6038,6th AIAA International Aerospace Plane and Hypersonics
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1 articles.
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