In this report a theory of thin airfoils of small camber is developed which permits either the velocity distribution corresponding to a given airfoil shape, or the airfoil shape corresponding to a given velocity distribution to be calculated. The procedures to be employed in these calculations are outlined and illustrated with suitable examples.
General theory of airfoil sections having arbitrary shape or pressure distribution
1945-01-01
Miscellaneous
No indication
English
General theory of airfoil sections having arbitrary shape or pressure distribution
Engineering Index Backfile | 1945
|Calculation of airfoil section with arbitrary pressure distribution
Engineering Index Backfile | 1938
|Engineering Index Backfile | 1951
|Theory of wing sections of arbitrary shape
TIBKAT | 1931
|Theory of wing sections of arbitrary shape
Engineering Index Backfile | 1931
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