Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow
Description: From Summary: "A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitrary plan form in incompressible flow is derived. The method requires that the span load at zero sideslip be known for the wing under consideration. Because this information is available for a variety of wings, this requirement should not seriously restrict the application of the present method. The basic method derived herein requires a mechanical differentiation and integration to obtain the rolling moment for the general wing in sideslip."
Date: October 6, 1955
Creator: Queijo, M. J.
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