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- W2005965638 abstract "An improvement on the enthalpy damping procedure currently in use in solving supersonic flow fields is described. A correction based on entropy values is shown to produce a very efficient scheme for simulation of high Mach number three-dimensional flows. Substantial improvements in convergence rates have been achieved by incorporating this enthalpy damping scheme in a finite-volume Runge-Kutta method for solving the Euler equations. Results obtained for blended wing-body geometries at very high Mach numbers are presented." @default.
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- W2005965638 date "1992-02-01" @default.
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- W2005965638 title "Enthalpy damping for high Mach number Euler solutions" @default.
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- W2005965638 doi "https://doi.org/10.2514/3.10917" @default.
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