A correction for Reynolds‐averaged‐Navier–Stokes turbulence model under the effect of shock waves in hypersonic flows-Reference-Cited by-同舟云学术

A correction for Reynolds‐averaged‐Navier–Stokes turbulence model under the effect of shock waves in hypersonic flows

Published:2022-10-08 Issue:2 Volume:95 Page:313-333
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Numerical Methods in Fluids

Author:

Tian Yuyan¹^ORCID,Gao Zhenxun¹,Jiang Chongwen¹,Lee Chun‐Hian¹

Affiliation:

1. School of Aeronautic Science and Engineering Beihang University Beijing China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/fld.5150

Reference40 articles.

1. DorseyJ PoteetC ChenR WursterK. Metallic thermal protection system technology development concepts requirements and assessment overview. Proceedings of the 40th AIAA Aerospace Sciences Meeting & Exhibit; Augest2002:502

2. HorstmanC.Prediction of hypersonic shock‐wave/turbulent‐boundary‐layer interaction flows. Proceedings of the 19th AIAA Fluid Dynamics Plasma Dynamics and Lasers Conference; June 1987:1367.

3. ManiM BabcockD WinklerC SpalartP.Predictions of a supersonic turbulent flow in a square duct. Proceedings of the 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition; January2003:860

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