Computational Studies of the Effects of Oxidizer Injector Length on Combustion Instability
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability
British Library Conference Proceedings | 2006
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