Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds

John DeYoung
Jul 1950

A simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line.

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