Numerical Investigation on HIFiRE-5 at Mach 6:Shockwave, Viscosity, and Cross Flow
21st AIAA International Space Planes and Hypersonics Technologies Conference
2017-01-01
Conference paper
Electronic Resource
English
Numerical Investigation on HIFiRE-5 at Mach 6:Shockwave, Viscosity, and Cross Flow (AIAA 2017-2380)
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