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
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
NTRS | 2008
|NTRS
|