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Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
作者:  Liang X;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy  
DNS of a spatially evolving hypersonic turbulent boundary layer at Mach 8 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 7, 页码: 1408-1418
作者:  Liang Xian;  Li XinLiang;  Liang X(梁贤)
浏览  |  Adobe PDF(1454Kb)  |  收藏  |  浏览/下载:899/322  |  提交时间:2013/06/13
Dns  Compressibility Effects  Turbulent Boundary Layer