Fuselage shape optimization of a wing-body configuration with nacelles
19th AIAA Applied Aerodynamics Conference ; 2001 ; Anaheim , CA , U.S.A.
01.01.2001
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Fuselage Shape Optimization of a Wing-Body Configuration with Nacelles
Online Contents | 2003
|AIAA-2001-2447 Fuselage Shape Optimization of a Wing-Body Configuration with Nacelles
British Library Conference Proceedings | 2001
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