This analysis computes for a predetermined airfoil and given Reynolds Number the course of the "displacement thickness," i.e., the course of the layer by which the streamlines of the potential flow are pushed away from the wing through the frictional layer. The result is, to a certain extent, a new wing contour.
Reduction of lift of a wing due to its drag
1935-11-01
Miscellaneous
No indication
English
Reduction of wing lift by the drag
TIBKAT | 1932
|Reduction of lift of wing due to its drag
Engineering Index Backfile | 1935
|Reduction of lift of a wing due to its drag
TIBKAT | 1935
|Crescent Wing Planforms Reduce Lift-Dependent Drag
NTRS | 1991
|Effect of wing tip strakes on wing lift-drag ratio
AIAA | 1989
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