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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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何国威 [6]
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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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Submit date:2017/12/18
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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Submit date:2016/01/08
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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Submit date:2015/03/17
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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Submit date:2014/11/03
Immersed Boundary Method
Leading-edge Vortices
Insect Flight
Aerodynamic Performance
Unsteady Aerodynamics
Wake Structure
Free Vortex
Bat Flight
Kinematics
Flow
An experimental investigation of dual-resonant and non-resonant responses for vortex-induced vibration of a long slender cylinder
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2014, 卷号: 57, 期号: 2, 页码: 321-329
Authors:
Wu XD(武晓东)
;
Ge F(葛斐)
;
Hong YS(洪友士)
;
Ge, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Submit date:2014/02/21
Vortex-induced Vibrations
Long Slender Cylinder
Dual-resonant Responses
Non-resonant Responses
An Improved Direct-Forcing Immersed Boundary Method for Fluid-Structure Interaction Simulations(1)
期刊论文
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2014, 卷号: 136, 期号: 4, 页码: 40903
Authors:
Zhu XJ(朱晓珏)
;
He GW(何国威)
;
Zhang X(张星)
;
Zhang, X(reprint author) Chinese Acad Sci, LNM, Inst Mech, Beijing 100190, Peoples R China
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Submit date:2014/04/18
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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Submit date:2013/11/18
Reynolds Number
Acceleration Terms
Control Volumes
Flapping Wing
Inertial Effect
Lamb Vectors
Low Reynolds Number
Separated Flows
Unsteady Lift
Second mode unstable disturbance measurement of hypersonic boundary layer on cone by wavelet transform
期刊论文
Acta Mechanica Sinica, 2011, 卷号: 27, 期号: 4, 页码: 488-493
Authors:
Han J
;
Jiang N(姜楠)
;
Tian Y
;
Han, J (reprint author), Tianjin Univ, Dept Math, Tianjin 300072, Peoples R China
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Submit date:2012/04/01
Hypersonic Boundary Layer
Sharp Cone
Instability
Wavelet Transform
Stability
Transition
Tunnel