Unsteady Shock Dynamics in Hypersonic Streamtraced Busemann Inlet at Sub-Design Mach Number and Varying Angles of Attack
AIAA SCITECH 2025 Forum
01.01.2025
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Investigation on a streamtraced hypersonic Busemann inlet
SAGE Publications | 2010
|Busemann inlet for hypersonic speeds.
AIAA | 1966
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