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The improvement of turbulence modeling for the aerothermal computation of hypersonic turbulent boundary layers

โœ Scribed by Ming Dong; Heng Zhou

Publisher
Science in China Press (SCP)
Year
2010
Tongue
English
Weight
716 KB
Volume
53
Category
Article
ISSN
1672-1799

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The applicability of a finite element-differential method to the computation of steady two-dimensional lowspeed, transonic and supersonic turbulent boundary-layer flows is investigated. The turbulence model chosen for the Reynolds shear stress and turbulent heat flux is the k-t. two-equation model.