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
01.01.2010
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
|The unsteady lift of a finite wing
TIBKAT | 1938
|Unsteady lift of wing of finite aspect ratio
Engineering Index Backfile | 1940
|