Efficient and robust Reynolds-stress model computation of three-dimensional compressible flows
JC Chassaing, GA Gerolymos, I Vallet - AIAA journal, 2003 - arc.aiaa.org
JC Chassaing, GA Gerolymos, I Vallet
AIAA journal, 2003•arc.aiaa.orgCourant–Friedrichs–Lewy numbers ofO (10–20) for the O (1–20) subiterations needed andO
(100–500) for the time marching. The robustness of the method is ensured by appropriate
positivity, boundedness, and Reynolds-stress realizability constraints. The numerical
method is illustrated by computing (and conducting numerical studies) for a high subsonic
(M» 0: 7) three-dimensional ow with large separation and for a transonic three-dimensional
shock-wave/boundary-layer interaction.
(100–500) for the time marching. The robustness of the method is ensured by appropriate
positivity, boundedness, and Reynolds-stress realizability constraints. The numerical
method is illustrated by computing (and conducting numerical studies) for a high subsonic
(M» 0: 7) three-dimensional ow with large separation and for a transonic three-dimensional
shock-wave/boundary-layer interaction.
Courant–Friedrichs–Lewy numbers ofO (10–20) for the O (1–20) subiterations needed andO (100–500) for the time marching. The robustness of the method is ensured by appropriate positivity, boundedness, and Reynolds-stress realizability constraints. The numerical method is illustrated by computing (and conducting numerical studies) for a high subsonic (M» 0: 7) three-dimensional ow with large separation and for a transonic three-dimensional shock-wave/boundary-layer interaction.
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