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A new supersonic rough-wall RANS model towards accurate drag and heat flux prediction

Yuhan WANG Zepeng YANG Xinliang GUO Wanli SHI Zhenxun GAO

中国航空学报（英文版）2026，Vol.39Issue(6)：56-72,17.

中国航空学报（英文版）2026，Vol.39Issue(6)：56-72,17.DOI:10.1016/j.cja.2025.103862

A new supersonic rough-wall RANS model towards accurate drag and heat flux prediction

Yuhan WANG ¹Zepeng YANG ¹Xinliang GUO ¹Wanli SHI ²Zhenxun GAO¹

作者信息

1. School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China
2. Aerodynamics Research Institute,Aviation Industry Corporation of China,Shenyang 110034,China
折叠

摘要

关键词

Roughness effect/Roughness function/Supersonic flow/Turbulent flow/Turbulence model

Key words

Roughness effect/Roughness function/Supersonic flow/Turbulent flow/Turbulence model

引用本文复制引用

Yuhan WANG,Zepeng YANG,Xinliang GUO,Wanli SHI,Zhenxun GAO..A new supersonic rough-wall RANS model towards accurate drag and heat flux prediction[J].中国航空学报（英文版）,2026,39(6):56-72,17.

基金项目

This study was supported by the National Natural Science Foundation of China(Nos.12372283 and U24B2007). （Nos.12372283 and U24B2007）

中国航空学报（英文版）

ISSN：1000-9361

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