The Interaction of Variable Duty Cycle Pulsed Injection and a Supersonic Shear Layer in a Scramjet Combustor
51st AIAA/SAE/ASEE Joint Propulsion Conference
2015-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2015
|Scramjet combustor wall boundary layer analysis
AIAA | 1981
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