Flow Separation Study in Stiff Ovalized Rocket Nozzles, Part II: Numerical Approach
51st AIAA/SAE/ASEE Joint Propulsion Conference
01.01.2015
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow Separation Study in Stiff Ovalized Rocket Nozzles, Part II: Numerical Approach (AIAA 2015-4154)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
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