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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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Indexed By:EI
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Numerical simulation of acoustic scattering and flow-induced noise with sharp interface immersed boundary method
会议论文
AIAA Scitech 2020 Forum, Orlando, FL, 2020/1/6-10
Authors:
Zhao C
;
Yang Y(杨焱)
;
Zhang T
;
Dong HB
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Submit date:2021/02/01
INVESTIGATION OF OBSTACLE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF FLAPPING WINGS
会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:
Yin B(银波)
;
Yang GW(杨国伟)
;
Yin, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
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Adobe PDF(6552Kb)
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View/Download:268/82
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Submit date:2018/01/16
Immersed-boundary Method
Micro-air Vehicles
Insect Flight
Vortices
Forces
Flows
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
Authors:
Liu TS
;
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
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View/Download:313/87
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Submit date:2016/01/07
On applicability of the Kutta-Joukowski theorem to low-Reynolds-number unsteady flows
会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
Authors:
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu TS
;
Wang SZ(王士召)
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Adobe PDF(755Kb)
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Submit date:2014/02/24
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300
会议论文
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
Authors:
Qi DW
;
He GW(何国威)
;
Liu YM
Adobe PDF(738Kb)
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View/Download:859/169
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Submit date:2013/02/26
Aerospace Engineering
Deformation
Exhibitions
Flexible Wings
Reynolds Number
Rigidity
Vortex Flow
Aerodynamic Forces
Chord-based Reynolds Number
Flexural Rigidities
Free Stream
Free-stream Flow
Lattice Boltzmann
Leading-edge Vortices
Lift Coefficient
Lift Force
Particle Methods
Pitch Rate
Power Efficiency
Reduced Frequency
Three Dimensional Space
Time-periods
Tip Edge
Trailing Edges
Trailing Vortex
Aerodynamic Performance of a Corrugated Dragonfly Airfoil Compared with Smooth Airfoils at Low Reynolds Numbers
会议论文
45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2007-1-8~2007-1-11
Authors:
Tama M
;
Wang ZJ
;
Rajagopalan G
;
Hu H
;
He GW(何国威)
Adobe PDF(4409Kb)
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Submit date:2012/02/13