A High Performance Aircraft Wind Tunnel Test Using Response Surface Methodologies
2005 U.S. Air Force T&E Days
2005-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hybrid Design for Aircraft Wind-Tunnel Testing Using Response Surface Methodologies
Online Contents | 2007
|Aerodynamic Parameters of High Performance Aircraft Estimated from Wind Tunnel and Flight Test Data
British Library Conference Proceedings | 1999
|Wind Tunnel Test on Models of V.T.O. Aircraft
Emerald Group Publishing | 1966
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