LES OF SHOCK-TURBULENT BOUNDARY LAYER INTERACTION OVER A MACH 10 HOLLOW CYLINDER WITH FLARE

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Veröffentlicht in:AIAA Aviation Forum (2021 : Online) Fluid dynamics ; Volume 1 of 2
1. Verfasser: Bhagwandin, Vishal A. (VerfasserIn)
Weitere Verfasser: Martin, Pino (VerfasserIn)
Pages:1
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
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