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Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3
作者:  Li GL(李广利);  Cui K(崔凯);  Xu YZ(徐应洲);  Wang HX(王浩祥);  Yang J(杨靖);  Xu XG(许先贵)
Adobe PDF(661Kb)  |  收藏  |  浏览/下载：359/82  |  提交时间：2020/05/18
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：308/95  |  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：411/120  |  提交时间：2018/10/30
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(763Kb)  |  收藏  |  浏览/下载：527/226  |  提交时间：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
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：295/95  |  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.
浏览  |  Adobe PDF(1218Kb)  |  收藏  |  浏览/下载：739/215  |  提交时间：2014/05/09
Group Velocity Control  Hybrid  Weno  Shockwave-turbulent Boundary Layer Interaction  Direct Numerical Simulation  
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods 期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
作者:  Lu HB(卢洪波);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Yue LJ(岳连捷)
浏览  |  Adobe PDF(1133Kb)  |  收藏  |  浏览/下载：905/257  |  提交时间：2014/04/15
Hypersonic Inlet  Cowl-lip Bluntness  Flow Characteristics  Shock Pattern  Shock Interference  
Effects of different product phases in aluminum dust detonation modeling 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 11, 页码: 2178-2185
作者:  Teng HongHui;  Jiang ZongLin;  Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(553Kb)  |  收藏  |  浏览/下载：724/252  |  提交时间：2013/11/18
Detonation  Aluminum  Multiphase  
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：877/258  |  提交时间：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust