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High-Pressure Capturing Wing Configurations 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:  Cui K(崔凯);  Li GL;  Xiao Y(肖尧);  Xu YZ;  Cui,K(reprint author), Chinese Acad Sci, Inst Mech
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Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
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, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(419Kb)  |  Favorite  |  View/Download：450/118  |  Submit date：2017/10/27
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:  Xiang GX(项高翔);  Wang C(王春);  Hu ZM(胡宗民);  Li XD;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(995Kb)  |  Favorite  |  View/Download：516/128  |  Submit date：2016/12/08
3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
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.
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Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
An integral heat flux sensor with high spatial and temporal resolutions 期刊论文
CHINESE SCIENCE BULLETIN, 2014, 卷号: 59, 期号: 27, 页码: 3484-3489
Authors:  Wu S(吴松);  Shu YH(舒勇华);  Li JP(李进平);  Yu HR(俞鸿儒);  Wu, S (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(652Kb)  |  Favorite  |  View/Download：699/232  |  Submit date：2014/09/23
Shock Tunnel  Heat Flux Sensor  Constantan Film  Electron Beam Co-evaporation  
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
Authors:  Dong M;  Li XL(李新亮);  Dong, M (reprint author), Tianjin Univ, Dept Mech, Tianjin 300072, Peoples R China
Adobe PDF(991Kb)  |  Favorite  |  View/Download：768/222  |  Submit date：2012/04/01
Turbulence Modeling  Supersonic  Hypersonic  Turbulent Boundary Layer  Dns  Bl Model  Direct Numerical-simulation  Temperature  Computation  Flows  
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Heating characteristics of blunt swept fin-induced shock wave turbulent boundary layer interaction 期刊论文
Acta Mechanica Sinica, 1998, 卷号: 14, 期号: 2, 页码: 139-146
Authors:  Tang GM(唐贵明);  Tang, GM (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100080, Peoples R China.
Adobe PDF(902Kb)  |  Favorite  |  View/Download：440/115  |  Submit date：2007/06/15