The NASA Ames 16-Inch Shock Tunnel nozzle simulations and experimental comparison
International Aerospace Planes and Hypersonics Technologies ; 1995 ; Chattanooga , TN , U.S.A.
1995-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Options for upgrade of the Ames 16-inch shock tunnel
AIAA | 1994
|Options for Upgrade of the AMES 16-Inch Shock Tunnel
British Library Conference Proceedings | 1994
|