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State Key... [14]
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何国威 [14]
张星 [10]
王士召 [7]
He GW [2]
Liu TS [2]
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Creator:何国威
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Document Type:会议论文
Community:非线性力学国家重点实验室
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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
Authors:
Liu TS
;
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
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Submit date:2016/01/07
Lateral migration of fiber in settling suspensions
会议论文
Paper Conference and Trade Show, PaperCon 2014, Nashville, TN, United states, April 26, 2014 - April 30, 2014
Authors:
Qi DW
;
He GW(何国威)
;
Liu YM
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Submit date:2017/05/27
Fiber Aspect Ratio
Fiber Suspensions
Lateral Migration
Lattice Boltzmann Simulations
Particle Densities
Particle Number Density
Repulsive Forces
Rotational Inertia
An improved direct-forcing immersed boundary method for fluid-structure interaction simulations
会议论文
ASME 2013 Fluids Engineering Division Summer Meeting, FEDSM 2013, Incline Village, NV, United states, JUL 07-11, 2013
Authors:
Zhang X(张星)
;
Zhu XJ(朱晓珏)
;
He GW(何国威)
;
Zhang X(张星)
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Submit date:2014/02/24
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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Submit date:2014/02/24
非预混燃烧中亚格子守恒标量FDF的双高斯分布及其先验检验
会议论文
中国力学大会——2013, 中国北京, 2013-08-19
Authors:
高福杰
;
张健
;
晋国栋
;
何国威
Adobe PDF(325Kb)
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Submit date:2014/04/02
预混燃烧
Fdf
高斯分布
标量
格子
湍流燃烧
化学反应速率
二元混合
直接数值模拟
预测效果
质量分数:函数:假设的:组分:较大的:0
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
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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
Spanwise stretching and collapse motions stabilize leading-edge vortex in slow-flying bats
会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:
Wang SZ(王士召)
;
He GW(何国威)
;
Zhang X(张星)
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Submit date:2014/04/02
Stretching
Stabilize
Flying
Leading
Collapse
Vortex
Oscillating
Stable
Slowing
Still
Simulate
Observed
Morphology
Around
Motion
Where
Taken
Method
Study
Aerodynamics of hovering flight in bat
会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:
Wang SZ(王士召)
;
He GW(何国威)
;
Zhang X(张星)
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Submit date:2014/04/02
Hovering
Flight
Generation
Inactive
Stokes
Simulation
Weight
Motion
Filed
Developed
Three
Evidence
Small
Deformation
An immersed boundary method based on the lattice Boltzmann approach in three dimensions, with application
会议论文
6th International Conference for Mesoscopic Methods in Engineering Science (ICMMES-09), Guangzhou, PEOPLES R CHINA, JUL 13-17, 2009
Authors:
Zhu LD
;
He GW(何国威)
;
Wang SZ(王士召)
;
Miller L
;
Zhang X(张星)
;
You Q
;
Fang SF
;
Zhu, LD (reprint author), Indiana Univ Purdue Univ, Dept Math Sci, Indianapolis, IN 46202 USA
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Submit date:2012/04/01
Immersed Boundary Method
Lattice Boltzmann Method
Fluid-structure Interaction
Deformable Body
Drag Scaling
Computational Fluid Dynamics
Incompressible Viscous Flow
Fluid-structure Interactions
Incompressible Viscous-flow
Finite-element-method
Level-set Method
Elastic Boundaries
Moving-boundaries
Simulating Fluid
Interface Method
Nonideal Gases
Flexible Fiber
AN IMMERSED BOUNDARY METHOD BASED ON NAVIER-STOKES EQUATIONS IN DISCRETE STREAM FUNCTION FORMULATION
会议论文
3rd Joint US-European Fluids Engineering Division Summer Meeting, Montreal, CANADA, AUG 01-05, 2010
Authors:
Zhang X(张星)
;
Wang SZ(王士召)
;
He GW(何国威)
;
Zhang, X (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
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Submit date:2016/06/28