A Suppression Method of Restricted Shock Separation in Overexpanded Rocket Nozzle
42nd, Joint propulsion conference & exhibit ; 2006 ; Sacramento, CA
2006-01-01
AIAA Paper 2006-4376
Paper numbers 2006-4300 to 2006-5277 with gaps held.; HELD ON CD-ROM
Conference paper
English
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Incident shock strength evolution in overexpanded jet flow out of rocket nozzle
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