An Integrated Aeroramp-Injector/Plasma-Igniter for Hydrocarbon Fuels in Supersonic Flow - Part B: Experimental Studies of the Operating Conditions
International conference; 10th, Space planes and hypersonic systems and technologies ; 2001 ; Kyoto, Japan
2001-01-01
10 pages
Contains papers AIAA-2001-1750 to 1927 only with gaps
Aufsatz (Konferenz)
Englisch
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