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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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PD-DEM hybrid modeling of leading edge erosion in wind turbine blades under controlled impact scenarios
期刊论文
COMPUTATIONAL PARTICLE MECHANICS, 2024, 页码: 19./通讯作者:Haeri, Sina
Authors:
Walayat, Khuram
;
Haeri, Sina
;
Iqbal, Imran
;
Zhang YH(张勇豪)
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View/Download:144/0
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Submit date:2024/04/15
Peridynamics
Discrete element method
Wind turbine blades
Leading edge erosion
Solid particle erosion
Damage
Crack
Wake of a bio-inspired flapping wing with morphing wingspan
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 10, 页码: 323061./通讯作者:Wang, SZ (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China., Wang, SZ (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 101408, Peoples R China.
Authors:
He XY(何心怡)
;
Liu Y(刘毅)
;
Chen YX(陈一鑫)
;
Wang SZ(王士召)
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Submit date:2023/07/17
Morphing wingspan
Wake structures
Flapping wing
Leading-edge vortex
Tip votices
Effect of the trailing-edge flap on tones due to self-excited oscillation within the leading-edge slat cove
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 卷号: 237, 期号: 4, 页码: 853-864./通讯作者:Guo, H (corresponding author), Beihang Univ, Inst Fluid Mech, Beijing 100191, Peoples R China.
Authors:
Lu WS(陆维爽)
;
Liu, Peiqing
;
Guo, Hao
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Submit date:2022/10/23
high-lift device
leading-edge slat
aerodynamic noise
acoustic characteristics
trailing-edge flap
Numerical study on near-field characteristics of landslide-generated impulse waves in channel reservoirs
期刊论文
JOURNAL OF HYDROLOGY, 2021, 卷号: 595, 页码: 13./通讯作者:Liu, Qingquan
Authors:
Wang, Xiaoliang
;
Shi CQ(石传奇)
;
Liu, Qingquan
;
An Y(安翼)
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Submit date:2021/06/21
Numerical simulation
Channel reservoir
Landslide-generated impulse waves
Near field
Leading wave
Comparative study of hybrid laser-MIG leading configuration on porosity in aluminum alloy bead-on-plate welding
期刊论文
INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2017, 卷号: 91, 期号: 5-8, 页码: 2681-2688
Authors:
Miao HB(苗海滨)
;
Yu G(虞钢)
;
He XL(何秀丽)
;
Li SX(李少霞)
;
Chen XY(陈旭阳)
;
Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Adv Mfg, Beijing 100190, Peoples R China.
;
Yu, G (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/08/15
Laser-mig Hybrid Welding
A7n01 Aluminum Alloy
Leading Configuration
Porosity
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
Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders
期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 207-217
Authors:
Wang FM(王发民)
;
Han HQ(韩汉桥)
;
Lei MF(雷麦芳)
;
Zhang J(张杰)
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Submit date:2015/09/24
Aerothermal Protection
Power-law Leading Edge
Aerodynamic Performance
Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders
会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:
Wang FM(王发民)
;
Han HQ(韩汉桥)
;
Lei MF(雷麦芳)
;
Zhang J(张杰)
;
Wang FM(王发民)
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Submit date:2014/03/11
Hypersonic
Aerothermal Protection
Power-law Leading Edge
Aerodynamic Performance
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