Effect of Upstream Boundary Layer on Unsteadiness of Swept-Ramp Shock/Boundary Layer Interactions at Mach 2 (AIAA 2016-0076)
Aerospace sciences meeting
01.01.2016
14 pages
Aufsatz (Konferenz)
Englisch
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Unsteadiness in Swept-Compression-Ramp Shock/Turbulent-Boundary-Layer Interactions (AIAA 2017-0987)
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