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Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
作者:  Chen XJ;  Qiu ZP;  Wang XJ;  Li YL;  Wang RX(王睿星)
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Uncertain Reduced-order Modeling  Robust Flutter Analysis  Interval Perturbation Method  Uncertain Aeroelastic System  
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
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Zhang DL(张德良);  Jiang ZL(姜宗林)
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Hypersonic  Aerodynamic Measurement  Theoretical Study  Vibration  
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
作者:  Li HX(李慧鑫);  Ye L(叶亮);  Wei XL(魏小林);  Li T(李腾);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
Explicit Role of Viscosity in Generating Lift 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 11, 页码: 3990-3994
作者:  Liu, Tianshu;  Wang SZ(王士召);  He GW(何国威);  Liu, TS (reprint author), Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA.
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Three-dimensional flame measurements with large field angle 期刊论文
OPTICS EXPRESS, 2017, 卷号: 25, 期号: 18, 页码: 21008-21018
作者:  Wang KL(王宽亮);  Li F(李飞);  Ceng H(曾徽);  Yu XL(余西龙);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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不同攻角下超声速降落伞伞绳的影响研究 期刊论文
航天返回与遥感, 2017, 卷号: 38, 期号: 04, 页码: 47-54
作者:  薛晓鹏;  温志湧;  汪运鹏;  张德良
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超声速降落伞  伞绳  攻角  数值模拟  着陆  
Influences of the helical strake cross-section shape on vortex-induced vibrations suppression for a long flexible cylinder 期刊论文
CHINA OCEAN ENGINEERING, 2017, 卷号: 31, 期号: 4, 页码: 438-446
作者:  Xu WH(徐万海);  Luan YS;  Liu LQ;  Wu YX(吴应湘)
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Helical Strakes  Viv Suppression  Cross-section Shape  Flexible Cylinder  
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
作者:  Huang CD(黄程德);  Liu W(刘文);  Yang GW(杨国伟)
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Aeroelasticity  Fluid-structure Interpolation  Grid Fin  Mesh Deformation  Radial Basis Function  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  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.
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Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
作者:  Tong FL(童福林);  Yu ZP(于长平);  Tang ZG(唐志共);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.;  Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation