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Explicit Role of Viscosity in Generating Lift 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 11, 页码: 3990-3994
Authors:  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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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
Authors:  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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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
Authors:  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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Lift enhancement by dynamically changing wingspan in forward flapping flight 期刊论文
PHYSICS OF FLUIDS, 2014, 卷号: 26, 期号: 6, 页码: 61903
Authors:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  He, GW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Immersed Boundary Method  Leading-edge Vortices  Insect Flight  Aerodynamic Performance  Unsteady Aerodynamics  Wake Structure  Free Vortex  Bat Flight  Kinematics  Flow  
Parallel computing strategy for a flow solver based on immersed boundary method and discrete stream-function formulation 期刊论文
COMPUTERS & FLUIDS, 2013, 卷号: 88, 页码: 210-224
Authors:  Wang SZ(王士召);  He GW(何国威);  Zhang X(张星);  Zhang, X (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
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Parallelization  Domain Decomposition  Massage Passing Interface  Immersed Boundary Method  Discrete Stream-function Formulation  
A lift formula applied to low-Reynolds-number unsteady flows 期刊论文
PHYSICS OF FLUIDS, 2013, 卷号: 25, 期号: 9, 页码: 093605/1-093605/22
Authors:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  He, GW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Reynolds Number  Acceleration Terms  Control Volumes  Flapping Wing  Inertial Effect  Lamb Vectors  Low Reynolds Number  Separated Flows  Unsteady Lift  
An immersed boundary method based on discrete stream function formulation for two- and three-dimensional incompressible flows 期刊论文
Journal of Computational Physics, 2011, 卷号: 230, 期号: 9, 页码: 3479-3499
Authors:  Wang SZ(王士召);  Zhang X(张星);  Zhang, X (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China
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Immersed Boundary Method  Discrete Stream Function Formulation  Incompressible Flow  Navier-stokes Equations  Parallel Computing  Large-eddy Simulation  Cartesian Grid Method  External Force-field  Low-reynolds-number  Circular-cylinder  Interface Method  Conservation Properties  Numerical-solutions  Moving Boundary  Viscous-flow