中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共8条，第1-8条 帮助

限定条件                    
已选(0)清除 条数/页：   排序方式：
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
作者:  Chen XP;  Li XL(李新亮);  Zhu ZC
浏览  |  Adobe PDF(1844Kb)  |  收藏  |  浏览/下载：312/98  |  提交时间：2019/04/11
direct numerical simulation  velocity-temperature correlation  supersonic flow  channel flow  thermally perfect gas  strong Reynolds analogy  
Hypersonic I-shaped aerodynamic configurations 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722
作者:  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ;  Li GL
浏览  |  Adobe PDF(665Kb)  |  收藏  |  浏览/下载：416/123  |  提交时间：2018/10/30
Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 6, 页码: 664702
作者:  Chen Z(陈哲);  Yu ZP(于长平);  Li L(李理);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1102Kb)  |  收藏  |  浏览/下载：300/97  |  提交时间：2016/09/14
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
作者:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(3301Kb)  |  收藏  |  浏览/下载：368/96  |  提交时间：2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Nonlinear spectral-like schemes for hybrid schemes 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2014, 卷号: 57, 期号: 4, 页码: 753-763
作者:  He, ZW;  Li XL(李新亮);  Liang X(梁贤);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1218Kb)  |  收藏  |  浏览/下载：744/217  |  提交时间：2014/05/09
Group Velocity Control  Hybrid  Weno  Shockwave-turbulent Boundary Layer Interaction  Direct Numerical Simulation  
Theoretical analysis of effects of boundary layer bleed on scramjet thrust 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
作者:  Yue LJ(岳连捷);  Xu XK(徐显坤);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(788Kb)  |  收藏  |  浏览/下载：878/258  |  提交时间：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust  
Towards an entropy-based detached-eddy simulation 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1970-1980
作者:  Zhao R(赵瑞);  Yan C(阎超);  Li XL(李新亮);  Kong WX;  Zhao, R (reprint author), Beijing Univ Aeronaut & Astronaut, Natl Lab Computat Fluid Dynam, Beijing 100191, Peoples R China.
Adobe PDF(1098Kb)  |  收藏  |  浏览/下载：1134/248  |  提交时间：2013/10/23
Hybrid Rans/les  Detached-eddy Simulation  Turbulence  Compressible Flows  Entropy  
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：901/323  |  提交时间：2013/06/13
Dns  Compressibility Effects  Turbulent Boundary Layer