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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
力学研究所 [2]
工程热物理研究所 [2]
长春光学精密机械与物... [1]
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OAI收割 [5]
内容类型
期刊论文 [3]
会议论文 [2]
发表日期
2023 [1]
2012 [2]
2004 [2]
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Wake of a bio-inspired flapping wing with morphing wingspan
期刊论文
OAI收割
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 10, 页码: 323061
作者:
He XY(何心怡)
;
Liu Y(刘毅)
;
Chen YX(陈一鑫)
;
Wang SZ(王士召)
|
收藏
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浏览/下载:27/0
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提交时间:2023/07/17
Morphing wingspan
Wake structures
Flapping wing
Leading-edge vortex
Tip votices
The load analysis of chisel-edge ruling tool for diffraction gratings (EI CONFERENCE)
会议论文
OAI收割
2012 International Applied Mechanics, Mechatronics Automation Symposium, IAMMAS 2012, September 7, 2012 - September 9, 2012, Shenyang, Liaoning, China
作者:
zhang f.
;
zhang f.
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浏览/下载:19/0
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提交时间:2013/03/25
The process of wear design on chisel-edge ruling tool of diffraction gratings is very complex because of following two reasons that one is the load distribution on minute edge area when grating ruling
and the other is the anisotropic character of natural diamond. The former is the first step when wear design on chisel-edge ruling tool of diffraction grating
In order to predicate the load distribution on minute edge area of tool
this paper simulated the load distribution on minute edge area of tool by software when ruling on Aluminum-1100 with tabular data format flow stress and Aluminum-1100 with Power law flow stress respectively
and through comparative analysis determined the approximate load distribution on minute edge area of chisel-edge ruling tool that the high load mainly focused on the edge area close to the tip of ruling tool and amount to 200MPa while about to 100MPa on the face of tool. (2012) Trans Tech Publications
Switzerland.
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
OAI收割
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
作者:
Qi DW
;
He GW(何国威)
;
Liu YM
收藏
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浏览/下载:60/0
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提交时间: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
Numerical Analysis and PIV Measurements of Tip Vortex in an Axial Rotor with Skewed-Swept Blade at Its Leading Edge
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2004, 卷号: 13, 期号: 1, 页码: 16,23
Guanghui Wu
;
Lijie Zheng
;
Keqi Wu
收藏
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浏览/下载:20/0
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提交时间:2013/03/11
axial rotor with skewed-swept blade at its leading edge
numerical simulation
tip vortex
PIV experiment
Numerical Analysis and PIV Measurements of Tip Vortex in an Axial Rotor with Skewed-Swept Blade at Its Leading Edge
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2004, 卷号: 13, 期号: 1, 页码: 16,23
作者:
Guanghui Wu
;
Lijie Zheng
;
Keqi Wu
|
收藏
|
浏览/下载:30/0
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提交时间:2013/03/11
Axial Rotor With Skewed-swept Blade At Its Leading Edge
Numerical Simulation
Tip Vortex
Piv Experiment
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