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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
Authors:  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.
View  |  Adobe PDF(763Kb)  |  Favorite  |  View/Download：552/232  |  Submit date：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
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
Authors:  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.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download：386/101  |  Submit date：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
Authors:  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.
View  |  Adobe PDF(1218Kb)  |  Favorite  |  View/Download：763/222  |  Submit date：2014/05/09
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
Authors:  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.
View  |  Adobe PDF(553Kb)  |  Favorite  |  View/Download：745/257  |  Submit date：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
Authors:  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)  |  Favorite  |  View/Download：889/263  |  Submit date：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust  
Shock tube study of kerosene ignition delay at high pressures 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2012, 卷号: 55, 期号: 6, 页码: 947-954
Authors:  Liang JH(梁金虎);  Wang S(王苏);  Hu HH(胡弘浩);  Zhang ST;  Fan BC(范秉诚);  Cui JP(崔季平);  Wang, S;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(690Kb)  |  Favorite  |  View/Download：754/260  |  Submit date：2013/01/18
Ignition Delay Time  Kerosene  Shock Tube  High Pressure  Mixtures  Autoignition  Temperatures  Times