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An airplane jig shape design method based on high fidelity aeroelastic simulation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
作者:  Yang W;  Wang QF;  Zhou L;  Zheng GN(郑冠男);  Liu W;  Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Aeroelasticity  Cfd  Csd  Jig Shape  Structural Mesh  
Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles 期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
作者:  Luo CT(罗长童);  Hu ZM(胡宗民);  Zhang SL;  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Aerodynamic Coefficient  Data Correlation  Scaling Parameter  Genetic Programming  Invariant  
Wave system fitting: A new method for force measurements in shock tunnels with long test duration 期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
作者:  Luo CT(罗长童);  Wang YP(汪云鹏);  Wang C(王春);  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Aerodynamic Force Measurements  Strain Gauge Balance  Inertia Compensation  Signal Decomposition  Accelerometer-free  Shock Tunnels  
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  
Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula 期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 6, 页码: 1492-1502
作者:  Liu TS;  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu, TS (reprint author), Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA.
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Numerical simulation of unsteady flows over a slow-flying bat 期刊论文
Theoretical and Applied Mechanics Letters, 2015, 卷号: 5, 页码: 5-8
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS
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The Lift Problem in Flapping Forward Flight at Low Reynolds Numbers 会议论文
53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida, USA, Jan 1-5,2015
作者:  Liu TS;  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威)
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Lift enhancement on spanwise oscillating flat-plates in low-Reynolds-number flows 期刊论文
Physics of Fluids, 2015, 卷号: 27, 期号: 6, 页码: 061901
作者:  Wang SZ(王士召);  He GW(何国威);  Zhang X(张星)
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Evaluation of Lift Formulas Applied to Low-Reynolds-Number Unsteady Flows 期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 1, 页码: 161-175
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  He, GW (reprint author), Chinese Acad Sci, State Key Lab Nonlinear Mech, Inst Mech, Beijing 100190, Peoples R China.
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Effects of a higher Reynolds number and introduced perforation on flows past the conic cylinder 会议论文
25th International Ocean and Polar Engineering Conference, ISOPE 2015, Kona, Big Island, HI, United states, June 21, 2015 - June 26, 2015
作者:  Lin LM(林黎明);  Zhong XF(钟兴福);  Wu YX(吴应湘)
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Circular Holes  Conic Disturbance  Disturbance Regime  Drag And Lift Coefficients  Hydrodynamic Parameters  Near Wake  Vortex Induced Vibration  Vortex Pattern