Mach reflection in steady supersonic flow considering wedge boundary-layer correction
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics ; 33 , 2
01.02.2020
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Mach Reflection of Shock and Detonation Waves in Steady Supersonic Chemically Reacting Flows
British Library Conference Proceedings | 2003
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