Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds
Description:
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. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedr…
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Date:
December 22, 1949
Creator:
DeYoung, John
Item Type:
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