Calibration of the New Mach 8 Nozzle at the AEDC Hypervelocity Wind Tunnel No. 9
25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA
Aerodynamic measurement technology and ground testing conference ; AIAA Paper 2006-2813-2006-2816
2006-01-01
AIAA Paper 2006-2813-2006-2816
Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference
Aufsatz (Konferenz)
Englisch
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The AEDC Hypervelocity Wind Tunnel 9
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|A NOVEL SIMULATION APPROACH FOR THE AEDC HYPERVELOCITY TUNNEL 9 MACH 14 NOZZLE
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