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- W2943865093 abstract "A vortex panel method has been developed to calculate the potentialflow about an arbitrary two dimensional aerofoil or axisymmetric shapeat fixed incidence in a steady, uniform, irrotational, incompressibleflow.The procedure replaces the contour by a suitably inscribed polygon,on which surface vorticity varies linearly and continuously along thepanel and is piecewise continuous at the panel corners.The Neumann boundary condition is satisfied at control pointssituated at the midpoint of each panel and the classical Kuttacondition is specified at the trailing edge by setting the netvorticity there equal to zero.This particular algorithm offers much flexibility in the treatmentof a greater range of aerofoil geometries and at higher incidence thanother surface singularity methods.Programme flow charts and FORTRAN code listings are given in theUser Guide (1)." @default.
- W2943865093 created "2019-05-16" @default.
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- W2943865093 date "1985-06-03" @default.
- W2943865093 modified "2023-09-23" @default.
- W2943865093 title "An Algorithm for the Calculation of the Potential Flow about an Arbitrary Two Dimensional Aerofoil. G.U. Aero Report 8502" @default.
- W2943865093 hasPublicationYear "1985" @default.
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