Optimization of Aircraft Configuration for Minimum Drag
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Optimization of Aircraft Configuration for Minimum Drag
British Library Conference Proceedings | 2010
|Ideal Tail Load for Minimum Aircraft Drag
AIAA | 1978
|