Effect of Maxwell gas-surface interaction models on flow characteristics and thermodynamic properties of rarefied hypersonic cavity flows

被引：0
|
作者：
Jin, Xuhong [1 ,2 ,3 ]
Huang, Fei [1 ,3 ]
Cheng, Xiaoli [1 ,3 ]
Su, Penghui [1 ,3 ]
机构：
[1] China Academy of Aerospace Aerodynamics, Beijing,100074, China
[2] School of Aerospace, Tsinghua University, Beijing,100084, China
[3] Laboratory of Aero-Thermal Protection Technology for Aerospace Vehicles (LAPTAV), China Aerospace Science and Technology Corporation (CASC), Beijing,100074, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 03期
基金：
中国国家自然科学基金;
关键词：
631.1 Fluid Flow; General - 641.2 Heat Transfer - 651.1 Aerodynamics; General; -; 652.1; Aircraft; 655.1; Spacecraft; General - 922.2 Mathematical Statistics;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
31
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