The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability
42nd, Joint propulsion conference & exhibit ; 2006 ; Sacramento, CA
2006-01-01
AIAA Paper 2006-4677
Paper numbers 2006-4300 to 2006-5277 with gaps held.; HELD ON CD-ROM
Aufsatz (Konferenz)
Englisch
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A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets
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