Direct numerical simulation techniques for hypersonic turbulent flows

被引：7
|
作者：
Li, Xinliang [1 ]
机构：
[1] State Key Laboratory of High-temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing,100190, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2015年 / 36卷 / 01期
关键词：
High resolution - High resolution scheme - High robustness - High temperature - Hypersonic turbulent flow - OpenCFD - Shock capture - Wall temperatures;
D O I：
10.7527/S1000-6893.2014.0233
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：147 / 158
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