WALL PRESSURE EFFECTS AND SHOCK-BOUNDARY LAYER INTERACTIONS IN A TRANSPIRATION COOLED SCRAMJET MODEL COMBUSTOR

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Veröffentlicht in:AIAA International Space Planes and Hypersonic Systems and Technologies Conference (23. : 2020 : Montréal) 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2020 ; Volume 2 of 2
1. Verfasser: Strauss, Friedolin T. (VerfasserIn)
Weitere Verfasser: Cragg, Stephan General. Patrick A. (VerfasserIn), Schlechtriem, Stefan (VerfasserIn)
Pages:23
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2020
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