An integrated aeroramp injector/plasma-igniter for hydrocarbon fuels in a supersonic flow. I - Experimental studies of the geometric configuration
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference ; 2001 ; Kyoto , Japan
2001-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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