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科研机构
北京航空航天大学 [3]
工程热物理研究所 [3]
北京大学 [2]
湖南大学 [2]
力学研究所 [1]
兰州理工大学 [1]
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期刊论文 [11]
会议论文 [3]
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2018 [3]
2017 [2]
2016 [3]
2013 [1]
2012 [2]
2010 [1]
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A new drag reduction method based on trailing vortex control by exhaust emissions
期刊论文
Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2018, 卷号: Vol.36 No.1, 页码: 47-51
作者:
Wen, Q.
;
Gu, Z.
;
Huang, T.
;
Chen, Z.
;
Tang, J.
收藏
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浏览/下载:8/0
  |  
提交时间:2019/12/26
Drag reduction
Exhaust emissions
Mini-bus
Trailing vortex
Wind tunnel test and gust load alleviation of flexible wing including geometric nonlinearities with servo control
会议论文
AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08
作者:
Chao, A.
;
Changchuan, X.
;
Yang, M.
;
Chao, Y.
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Aspect ratio
Atmospheric turbulence
Aviation
Control nonlinearities
Control surfaces
Finite element method
Flexible wings
Linearization
Proportional control systems
State space methods
Structural dynamics
Two term control systems
Wind stress
Geometric non-linearity
Gust load alleviation
Nonlinear finite element method
Proportional integral derivative controllers
State - space models
Trailing-edge control surfaces
Vertical accelerations
Vortex lattice method
Wind tunnels
Application of the vortex effects induced by the trailing wedge to enhance the mixing and combustion in the strut-based scramjet
期刊论文
APPLIED THERMAL ENGINEERING, 2018, 卷号: 140, 页码: 604-614
作者:
Zhu, Shaohua
;
Xu, Xu
;
Yang, Qingchun
收藏
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浏览/下载:5/0
  |  
提交时间:2019/12/30
Strut-based scramjet
Fuel-air mixing
Trailing wedge
Vortex effects
Numerical simulation
Numerical study on the effect of the diffuser blade trailing edge profile on flow instability in a nuclear reactor coolant pump
期刊论文
NUCLEAR ENGINEERING AND DESIGN, 2017, 卷号: 322, 页码: 92-103
作者:
Ni, Dan[1]
;
Yang, Minguan[2]
;
Gao, Bo[3]
;
Zhang, Ning[4]
;
Li, Zhong[5]
收藏
  |  
浏览/下载:14/0
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提交时间:2019/12/24
Nuclear reactor coolant pump (RCP)
Diffuser blade trailing edge (BTE)
Vortex shedding
Flow instability
Prediction of vortex-shedding noise from the blunt trailing edge of a flat plate
期刊论文
JOURNAL OF SOUND AND VIBRATION, 2017, 卷号: 408, 页码: 20-30
作者:
Wu, Long
;
Jing, Xiaodong
;
Sun, Xiaofeng
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Trailing edge
Vortex shedding
Bluntness
Discrete vortex model
Acoustic perturbation equations
Noise prediction
Numerical Study of Improving Aerodynamic Performance of Low Solidity LPT Cascade through Increasing Trailing Edge Thickness
期刊论文
2016
作者:
Li, C., Yan, P. G., Wang, X. F., Han, W. J. and Wang, Q. C.
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浏览/下载:40/0
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提交时间:2017/05/27
Aircraft engine low pressure turbine trailing edge thickness profile loss flow control vortex-generator jets separation control local variables
Numerical Study of Combining Steady Vortex Generator Jets and Deflected Trailing Edge to Reduce the Blade Numbers of Low Pressure Turbine Stage
期刊论文
2016
作者:
Li, C., Yan, P. G., Wang, X. F., Han, W. J. and Wang, Q. C.
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浏览/下载:22/0
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提交时间:2017/05/27
low pressure turbine
profile loss
flow control
Vortex Generator Jets
deflected trailing edge
separation control
local variables
part i transition
Research on Non-smooth Surfaces for Control of the Automobile Trailing Vortex Structure
期刊论文
Journal of Mechanical Engineering, 2016, 卷号: Vol.52 No.8, 页码: 133-140
作者:
Yang Yi
;
Huang Jianfeng
;
Fan Guanghui
;
Cai Shengkang
;
Liu Zheng
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/31
car body
non-smooth surface
wind tunnel test
trailing vortex
disturbance effect
aerodynamic characteristics
The passive control of wake flow behind a circular cylinder by parallel dual plates
期刊论文
journal of fluids and structures, 2013
Bao, Y.
;
Tao, J.
收藏
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浏览/下载:6/0
  |  
提交时间:2015/11/12
Drag reduction
Wake suppression
Splitter plate
VORTEX-INDUCED VIBRATION
LOW REYNOLDS-NUMBERS
BLUNT TRAILING-EDGE
SPLITTER PLATES
DRAG REDUCTION
BLUFF-BODY
2-DIMENSIONAL FLOW
SUPPRESSION
BODIES
FORCES
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
作者:
Qi DW
;
He GW(何国威)
;
Liu YM
收藏
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浏览/下载:49/0
  |  
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
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