Effects of Surface Compliance on Shock Boundary Layer Interaction in the Caltech Mach 4 Ludwieg Tube
Author:
Affiliation:
1. California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Reference19 articles.
1. Fluid-Structure Interactions on a Slender Cone under Quiet Flow Conditions at Mach 6
2. Measurement and simulation of hypersonic fluid-structural interaction on a cantilevered plate in a Mach 6 flow
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4. Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions
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