Computational and Experimental Characterization of the Mach 6 Facility Nozzle Flow for the Enhanced Injection and Mixing Project at NASA Langley Research Center (AIAA 2017-1537)
55th AIAA Aerospace Sciences Meeting 2017 ; 2017 ; Grapevine, Texas
2017-01-01
27 pages
Aufsatz (Konferenz)
Englisch
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