Effect of gap size on pressure and heating over the flap of a blunt delta wing in hypersonic flow.
Author:
Affiliation:
1. Martin Marietta Corporation, Baltimore, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28818
Reference7 articles.
1. Mach 8 to 22 studies of flow separations due to deflected control surfaces
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