Optimization of Aircraft Configuration for Minimum Drag
51st, AIAA/ASME/ASME/ASCE/AHS/ASC Structures, Stuctural Dynamics and Materials Conference ; 2010 ; Orlando, FL
2010-01-01
9 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Optimization of Aircraft Configuration for Minimum Drag
AIAA | 2010
|Ideal Tail Load for Minimum Aircraft Drag
AIAA | 1978
|