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Applied Mathematical Modelling
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Applied Mathematical Modelling
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Computational analysis of supersonic turbulent boundary layers over rough surfaces using the k–ω and the stress–ω models

Computational analysis of supersonic turbulent boundary layers over rough surfaces using the \(k\)-\(\omega \) and the stress-\(\omega\) models
descriptionPublicationkeyboard_double_arrow_right Article 01 Dec 2007 English Publisher:Elsevier BVJournal:Applied Mathematical Modelling, volume 31, pages 2,655-2,667 (issn: 0307-904X, Copyright policy )
Authors: Sharif, M. A. R.; Guo, G.;

doi: 10.1016/j.apm.2006.10.007

Computational analysis of supersonic turbulent boundary layers over rough surfaces using the k–ω and the stress–ω models

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Keywords

turbulence models, \(k\)-\(\varepsilon\) modeling in turbulence, Turbulent boundary layers, Modelling and Simulation, Applied Mathematics, Supersonic flows, surface roughness, \(k\)-\(\omega\) and stress-\(\omega \) models, supersonic boundary layer flow

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
5
Average
Average
Average
hybrid