Computational Flow Simulations of Overexpanded Rocket Nozzle Flowfields including Unsteady Effects
European symposium; 4th, Aerothermodynamics for space vehicles ; 2001 ; Capua, Italy
01.01.2002
8 pages
One CD-ROM in pocket attached to inside back cover
Aufsatz (Konferenz)
Englisch
aerothermodynamics , space vehicles , ESA , CIRA , ASI
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Incident shock strength evolution in overexpanded jet flow out of rocket nozzle
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