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Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download：293/63  |  Submit date：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Shock oscillation in highly underexpanded jets 期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 9, 页码: 94705
Authors:  Li XP;  Zhou R;  Chen XP;  Fan XJ(范学军);  Xie GS
View  |  Adobe PDF(8162Kb)  |  Favorite  |  View/Download：326/91  |  Submit date：2018/10/30
highly underexpanded jets  shock oscillation  large eddy simulation  
Aerodynamic measurement of a large aircraft model in hypersonic flow 期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Zhang DL(张德良);  Jiang ZL(姜宗林)
View  |  Adobe PDF(4916Kb)  |  Favorite  |  View/Download：493/115  |  Submit date：2017/12/18
Hypersonic  Aerodynamic Measurement  Theoretical Study  Vibration  
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：398/105  |  Submit date：2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(532Kb)  |  Favorite  |  View/Download：653/158  |  Submit date：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp 期刊论文
SCIENCE CHINA: Physics, Mechanics & Astronomy, 2010, 卷号: 53, 期号: 9, 页码: 1651-1658
Authors:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Liang X(梁贤);  Li XL(李新亮)
View  |  Adobe PDF(951Kb)  |  Favorite  |  View/Download：1620/369  |  Submit date：2010/10/25
compression Ramp  Shock/turbulent Boundary Layer Interaction  Direct Numerical Simulation  Shock Oscillation  
Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow 期刊论文
Chinese Physics Letters, 2009, 卷号: 26, 期号: 9, 页码: 094701-1-4
Authors:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Gao H(高慧)
Adobe PDF(1149Kb)  |  Favorite  |  View/Download：1099/321  |  Submit date：2010/03/07
Direct Numerical-simulation  Sound