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
01.01.1945
Sonstige
Keine Angabe
Englisch
General theory of airfoil sections having arbitrary shape or pressure distribution
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