Control Theory Based Airfoil Design using the Euler Equations
5th AIAA/USAF/NASA/ISSMO symposium, Multidisciplinary analysis and optimization ; 1994 ; Panama City Beach; FL
01.01.1994
17 pages
In 2 pts
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA | 1984
|Computation of the Flows over Flapping Airfoil by the Euler Equations
British Library Conference Proceedings | 2005
|