Developing Response Surface Based Wing Weight Equations for Conceptual Morphing Aircraft Sizing
46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Conceptual Morphing Aircraft Sizing Using a Multi-Level Optimization Strategy
British Library Conference Proceedings | 2008
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