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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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Design and characterization for dual-band and multi-band A sandwich composite radome walls
期刊论文
COMPOSITES SCIENCE AND TECHNOLOGY, 2017, 卷号: 149, 页码: 28-33
Authors:
Zhou, Licheng
;
Wang, Peiyu
;
Pei, Yongmao
;
Zeng, Anmin
;
Tang, Liqun
;
Liu, Zejia
;
Liu, Yiping
;
Jiang, Zhenyu
;
Fang, Daining
;
Pei, YM (reprint author), Peking Univ, Coll Engn, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China.
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View/Download:365/156
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Submit date:2017/11/29
Radome
Dual-band
Multi-band
Sandwich Structure
Transmission
Self-propelled swimming of a flexible plunging foil near a solid wall
期刊论文
BIOINSPIRATION & BIOMIMETICS, 2016, 卷号: 11, 期号: 4, 页码: 46005
Authors:
Dai LZ
;
He GW(何国威)
;
Zhang X(张星)
;
Zhang, X (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Submit date:2016/07/11
Wall Effect
Self-propulsion
Flapping Foil
Flexibility
Biolocomotion
Research on the mechanics of high speed rails
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 189-190
Authors:
Wei YJ(魏宇杰)
;
Wei, YJ (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
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Submit date:2017/12/18
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
Lattice Boltzmann simulations of a pitch-up and pitch-down maneuver of a chord-wise flexible wing in a free stream flow
期刊论文
PHYSICS OF FLUIDS, 2014, 卷号: 26, 期号: 2, 页码: 21902
Authors:
Qi, Dewei
;
He GW(何国威)
;
Liu, Yingming
;
Qi, DW (reprint author), Western Michigan Univ, Dept Chem & Paper Engn, Kalamazoo, MI 49008 USA.
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Submit date:2014/05/09
Three-point Velocity Correlation
Turbulence
Large Eddy Simulation
Velocity Increment
Multiscale Analysis
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