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Arbitrary Configurations boundary layer Buttline Cut Comparison of Calculated component computed control point datum solutions Dirichlet boundary condition doublet distribution equation evaluated external Neumann boundary flap flow field formulation fuselage geometry ground effect input internal Dirichlet boundary internal flow iteration loop jump Kutta Kutta condition low-order panel methods lower surface Maskew mean plane Metroliner Wind Tunnel NACA nacelle NASA neighboring panels Neumann boundary condition normal velocity onset flow Panel Neighbors perturbation velocity plane of symmetry Position vector Potential Flow present calculations Pressure Distributions problem quadrilateral region Section singularity distributions source distribution source term spanwise specified Subroutine Subsection surface and wake Surface Integrals surface panels Swearingen Metroliner Wind Swept Wing tangent vector tion trailing edge upper and lower velocity potential influence velocity vector VSAERO program wake column wake lines wake panels wake surface wake-grid plane wake-shape Wind Tunnel Model wing wing-body zero