Compression Ramp Induced Shock-Wave/Turbulent Boundary-Layer Interactions on a Compliant Material
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695
Funder
Air Force Office of Scientific Research
Army Research Office
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056652
Reference17 articles.
1. Possibilities of drag reduction by the use of flexible skin.
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3. Shock induced fluid-structure interaction on a flexible wall in supersonic turbulent flow
4. BOUNDARY LAYER STABILIZATION BY DISTRIBUTED DAMPING
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