Publication: Effects of Double-Wedge Aft Angle on Hypersonic Laminar Flows
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American Institute of Aeronautics and Astronautics (AIAA)
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Abstract
The aim of this study is to reveal the physics of low-enthalpy Mach 7 flows over double wedges that have varied aft angles and a fixed fore angle of 30°. Comparisons of the obtained numerical schli...
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AIAA Journal
ISSN
0001-1452
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OPEN