Maximum Lift of the Wing Shape Bodies for Unsteady Motion Converges to About CL=2.5
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
2010-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
MAXIMUM LIFT OF THE WING SHAPE BODIES FOR UNSTEADY MOTION CONVERGES TO ABOUT C~L=2.5
British Library Conference Proceedings | 2010
|Engineering Index Backfile | 1939
|The unsteady lift of a finite wing
SLUB | 1938
|Unsteady lift of wing of finite aspect ratio
Engineering Index Backfile | 1940
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