Theory of thin airfoils of small camber developed which permits either velocity distribution corresponding to given airfoil shape, or airfoil shape corresponding to given velocity distribution to be calculated; procedures to be employed are outlined and illustrated with suitable examples. (20¢) (released 1948)
General theory of airfoil sections having arbitrary shape or pressure distribution
Nat Advisory Committee Aeronautics -- Report
1945
23 pages
Bibliography
Report
English
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Calculation of airfoil section with arbitrary pressure distribution
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