HYPERSONIC SHOCK WAVE-BOUNDARY-LAYER INTERACTION ON THE CONTROL SURFACE OF A SLENDER CONE

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 3 of 7
1. Verfasser: Pandey, Anshuman (VerfasserIn)
Weitere Verfasser: Casper, Katya M. (VerfasserIn), Spillers, Russell (VerfasserIn), Soehnel, Melissa (VerfasserIn), Spitzer, Seth (VerfasserIn)
Pages:3
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Sprache:eng
Veröffentlicht: 2020
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