Design of Aerothermoelastic Experiments in the AFRL Mach 6 High Reynolds Number Facility
Author:
Affiliation:
1. Air Force Research Laboratory
2. ARCTOS, LLC
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0948
Reference32 articles.
1. Stillwell, W. “X-15 Research Results with a Selected Bibliography,” Technical Report NASA-SP-60, October 1965.
2. Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions
3. Experiments on a Thin Panel Excited by Turbulent Flow and Shock/Boundary-Layer Interactions
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