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Solution to the Compressible Navier-Stokes Equations of Motion by Chebyshev Polynomials with Implicit Time Stepping

机译:用隐式时间步进的Chebyshev多项式求解可压缩Navier-stokes运动方程

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Implicit time stepping has been incorporated into the author's pseudospectral compressible Navier-Stokes code. This report presents results for three classes of laminar flows. A normal shock wave laminar boundary layer interaction on a flat plate, an oblique shock wave laminar boundary layer interaction on a flat plate and the flow over a circular arc airfoil at two mach numbers. Keywords: Airfoils; Inviscid time dependent compressible flow; Euler equations of motion.

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