Supersonic turbulent flow past a 3-D swept compression corner at Mach 3

Knight, Doyle; Horstman, C. C.; Ruderich, R.; Mao, Marlon; Bogdonoff, S. M.

doi:10.2514/6.1987-551

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Comment On "New Eddy Viscosity Model For Computation Of Swir1

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1991

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Cited by 13 publications

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“…Kim and Chung implemented the k-e model by deriving an algebraic equation for eddy viscosity based on the algebraic Reynolds stress model proposed by Rodi. 5 In Rodi's model, the equation is…”

Section: Comment On "New Eddy Viscosity Model For Computation Of Swirmentioning

confidence: 99%

Reply by Author to C.-M. Hung

Ericsson

1991

AIAA Journal

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READERS' FORUM 1023and cases 1-3 in Ref. 2. One can speculate that for the case of supersonic flow over a blunt fin, 4 at least in the region ahead of the blunt fin, the flow is strongly dominated by the geometry and other inviscid mechanisms. The strength of the primary vortex was closely predicted; hence so were the main features. For the case of supersonic flow over a swept corner, 2 the mechanism for generating the primary vortex was probably not correctly simulated; hence so were not the strength of the vortex and its associated'features.

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Section: Comment On "New Eddy Viscosity Model For Computation Of Swirmentioning

confidence: 99%