Input/output Analysis of a Mach-6 Cooled-wall Hypersonic Boundary Layer Using the One-Way Navier-Stokes (OWNS) Equations

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Veröffentlicht in:AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Fluid dynamics ; Volume 2 of 3
1. Verfasser: Kamal, Omar (VerfasserIn)
Weitere Verfasser: Rigas, Georgios (VerfasserIn), Lakebrink, Matthew T. (VerfasserIn), Colonius, Tim (VerfasserIn)
Pages:2
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Sprache:eng
Veröffentlicht: 2022
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