TRANSIENT SHOCK WAVE INTERACTION WITH ROCKET NOZZLE - COLD-FLOW STUDY
39th, Joint propulsion conference; 39th AIAA/ASME/SAE/ASEE joint propulsion conference ; 2003 ; Huntsville, AL
01.01.2003
4669 pages
Nos 2003-4404 to 2003-9731 with gaps
Aufsatz (Konferenz)
Englisch
AIAA , ASME , SAE , ASEE , propulsion , aeronautics , automotive engineers , mechanical engineers , joint propulsion
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