Improved γ-Re model for heat transfer prediction of hypersonic boundary layer transition-Reference-Cited by-同舟云学术

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Improved γ-Re model for heat transfer prediction of hypersonic boundary layer transition

Published:2017-04 Issue: Volume:107 Page:329-338
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Hao Zihui,Yan Chao,Qin Yupei,Zhou Ling

Funder

National Laboratory for Computational Fluid Dynamics

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference24 articles.

1. Large eddy simulation of unsteady transitional flow on the low-pressure turbine blade;Wang;Sci. China,2014

2. Turbulence models for near-wall and low Reynolds number flows: a review;Patel;AIAA J.,2012

3. Turbulence Modelling for CFD;Wilcox,1992

4. A three-equation eddy-viscosity model for Reynolds-averaged Navier-Stokes simulations of transitional flow;Walters;J. Fluids Eng.,2008

5. Modelling flow transition in a hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach;Wang;Sci. China-Phys. Mech. Astron.,2009

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2. Gas Kinetic Scheme Coupled with High-Speed Modifications for Hypersonic Transition Flow Simulations;Entropy;2024-02-18

3. Local correlation, compressibility, and crossflow corrections of γ-Reθ transition model for high-speed flows;Physics of Fluids;2024-01-01

4. A Study on Optimal Geometry of Scramjet 2D Intake Considering Viscous Boundary Layer and Transition Phenomena;Journal of the Korean Society for Aeronautical & Space Sciences;2023-09-30

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