AIAA-2001-2447 Fuselage Shape Optimization of a Wing-Body Configuration with Nacelles
Conference; 19th, Applied aerodynamics ; 2001 ; Anaheim, CA
01.01.2001
7 pages
Separate papers 2001-2401 to 2001-2485 with gaps
Aufsatz (Konferenz)
Englisch
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Fuselage Shape Optimization of a Wing-Body Configuration with Nacelles
Online Contents | 2003
|AIAA-2001-2482 Aerodynamic Evaluation of Wing Tip Mounted Nacelles
British Library Conference Proceedings | 2001
|