## The spanwise lift distribution of swept wings at subsonic speeds |

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account for compressibility additional loading Aeronautical Engineering airfoils angle of attack aspect ratio assumed basic loading Bound or Load bound vortices calculations camber circular coordinate circulation computed control points chosen CORNELL UNIVERSITY correction factor DeToung and Harper DeYoung downwash contribution downwash due experimental data experimental results expressed functions gives Harper Ref high angles incompressible flow indicated infinity integral Interpolation coefficients lateral coordinate lift curve slope lifting surface theories line0 load vortex Mach number mathematical analysis mathematical solution matrix coefficient NACA TN Nondimensionalizing number of control plane of symmetry planforms plate Prandtl predict pressure measurements quadrature formula quarter chord line resulting downwash angle semispan Sheet of Trailing Span Load Characteristics spanwise lift distribution spanwise loading spanwise stations Subsonic sweepback swept wing symmetric loading Table term theoretical values three quarter chord trailing vortex sheet Trefftz plane twist unswept vortex line Weissinger method wing geometry wing lift coefficient zero net lift