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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:531/227  |  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: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.
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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.
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Group Velocity Control  Hybrid  Weno  Shockwave-turbulent Boundary Layer Interaction  Direct Numerical Simulation  
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:729/253  |  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: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  
A 5th order monotonicity-preserving upwind compact difference scheme 期刊论文
Science China, Physics, Mechanics & Astronomy, 2011, 卷号: 54, 期号: 3, 页码: 511-522
作者:  He ZW(何志伟);  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Li, XL (reprint author), Chinese Acad Sci, Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China
浏览  |  Adobe PDF(725Kb)  |  收藏  |  浏览/下载:820/229  |  提交时间:2012/04/01
Upwind Compact Scheme  Monotonicity-preserving  Compressible Flows  Shock Capturing Scheme  Hyperbolic Conservation-laws  Essentially Nonoscillatory Schemes  Shock-turbulence Interaction  High-resolution Schemes  High-order  Efficient Implementation  Flow  
Problems of the conventional BL model as applied to super/hypersonic turbulent boundary layers and its improvements 期刊论文
Science China-Physics Mechanics & Astronomy, 2011, 卷号: 54, 期号: 10, 页码: 1889-1898
作者:  Dong M;  Li XL(李新亮);  Dong, M (reprint author), Tianjin Univ, Dept Mech, Tianjin 300072, Peoples R China
Adobe PDF(991Kb)  |  收藏  |  浏览/下载:741/214  |  提交时间:2012/04/01
Turbulence Modeling  Supersonic  Hypersonic  Turbulent Boundary Layer  Dns  Bl Model  Direct Numerical-simulation  Temperature  Computation  Flows