Steady Turbulent Flow Computations Using a Low Mach Fully Compressible Scheme

A recently proposed modification to fully compressible schemes significantly improves the resolution of low-Mach-number features, tackling the problem of excessive numerical dissipation as the Mach number reduces. This paper explores the application of this modification to Reynolds-averaged Navier–S...

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Veröffentlicht in:	AIAA journal 2014-11, Vol.52 (11), p.2559-2575
Hauptverfasser:	Garcia-Uceda Juarez, A, Raimo, A, Shapiro, E, Thornber, B
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace engineering Backward facing steps Boundary layer interaction Compressibility Computation Computational fluid dynamics Fluid dynamics Fluid flow Holes Mach number Mathematical models Navier-Stokes equations Numerical dissipation Oblique shock waves Solvers Turbulence Turbulent flow
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