DESIGN OPTIMIZATION OF ROCKET BASED COMBINED CYCLE INLET/EJECTOR SYSTEM
39th, Joint propulsion conference; 39th AIAA/ASME/SAE/ASEE joint propulsion conference ; 2003 ; Huntsville, AL
2003-01-01
5232 pages
Nos 2003-4404 to 2003-9731 with gaps
Conference paper
English
AIAA , ASME , SAE , ASEE , propulsion , aeronautics , automotive engineers , mechanical engineers , joint propulsion
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