Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel
20th AIAA Advanced Measurement and Ground Testing Technology Conference ; 1998 ; Albuquerque , NM , U.S.A.
1998-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Supersonic Retropropulsion Experimental Results from NASA Ames 9 × 7 Foot Supersonic Wind Tunnel
Online Contents | 2014
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