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PREFACE by W G Habashi I
Numerical Algorithms for Transonic Inviscid
16 other sections not shown
accuracy aerodynamic AIAA Journal AIAA Paper airfoil algorithm analysis applied approximation boundary conditions cell characteristic coefficient compressible Computational Fluid Dynamics contour coordinate defined density developed differencing discontinuities discrete downstream embedded mesh entropy Euler equations explicit Figure finite difference finite element flow field Fluid Dynamics flux formulation full potential equation governing equations grid points inlet integration interpolation inviscid isentropic iteration Jameson Kutta condition lift coefficient linear Mach number matrix method multigrid multiple-grid NACA NASA nonlinear obtained operator physical potential flow present pressure distribution procedure region second order second-order shock wave shown in Fig solve solver sonic spectral spectral method speed stability stagnation point steady Steger step stream function streamline subsonic supercritical supersonic surface techniques three-dimensional tion trailing edge Transonic Potential Flow two-dimensional Unsteady Transonic Flow upstream upwind variables vector velocity velocity potential viscosity vorticity wing zero