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科研机构
北京航空航天大学 [7]
内容类型
期刊论文 [5]
会议论文 [2]
发表日期
2018 [7]
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发表日期:2018
专题:北京航空航天大学
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A fast estimation of shock wave pressure based on trend identification
期刊论文
MEASUREMENT SCIENCE AND TECHNOLOGY, 2018, 卷号: 29
作者:
Yao, Zhenjian
;
Wang, Zhongyu
;
Wang, Chenchen
;
Lv, Jing
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
shock wave pressure
dynamic measurement
discrete cosine transform
trend identification
shock tube
Flap upward deflection and rearward bump combination to alleviate transonic buffet of supercritical wing
会议论文
AIAA Aerospace Sciences Meeting, 2018, 2018-01-08
作者:
Gao, S.
;
Yun, T.
;
Liu, P.
;
Qu, Q.
收藏
  |  
浏览/下载:12/0
  |  
提交时间:2019/12/30
Airfoils
Aviation
Adverse pressure gradient
Drag prediction
Flow condition
Separation bubble
Shock wave oscillation
Supercritical airfoils
Trailing edge flaps
Transonic buffet
Shock waves
Experimental Research about Shock Wave in a 1+1/2 Counter-Rotating Turbine
会议论文
2017 ASIA CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ACMAE 2017), 2018-01-01
作者:
Li, Chao
;
Liu, Huo-Xing
;
Zhou, Zhi-Hong
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
Aerospace engineering
Computational fluid dynamics
Flow fields
Shock waves
Turbines
Turbomachine blades
Wakes
Wind tunnels
1+1/2 counter-rotating turbines
Distribution regularities
Expansion ratio
Experimental research
Shock-wave structures
Supersonic wind tunnel
Unsteady effects
Wave structures
High pressure effects
Large-eddy simulation of MVG controlled oblique shockwave/turbulent boundary layer interaction [MVG控制斜激波/湍流边界层干涉的大涡模拟]
期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 1639-1646
作者:
Yang, G.
;
Fang, J.
;
Lu, L.
;
Yao, Y.
;
Liu, C.
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Aerodynamics
Boundary layer flow
Boundary layers
Flow control
Flow fields
Shear flow
Shear stress
Shock waves
Vortex flow
Vorticity
Wakes
Boundary layer interaction
Boundary-layer separation
Immersed boundary methods
Kelvin-helmholtz instabilities
Micro vortex generators
Shock-wave/boundary layer interactions
Stream-wise velocities
Turbulent boundary layers
Large eddy simulation
Control of compression ramp flow separation via vane vortex generator [叶片式涡流发生器对压缩拐角流动分离的控制]
期刊论文
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2018, 卷号: 39
作者:
Hu, W.
;
Yu, J.
;
Liu, H.
;
Zhao, Y.
;
Yan, C.
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2019/12/30
Acoustic streaming
Boundary layers
Drag
Flow separation
Hypersonic flow
Navier Stokes equations
Rotating machinery
Shock waves
Turbomachine blades
Turbulence models
Vorticity
Boundary-layer separation
Compression ramps
Shock wave boundary layer interactions
Streamwise vortices
Vortex generators
Vortex flow
Nonsteady Shock Wave Attenuation Due to Leakage
期刊论文
ENERGIES, 2018, 卷号: 11
作者:
Liu, Chenyuan
;
Liu, Huoxing
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  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
gas turbine
wave rotor
leakage
shock wave
Euler equations
initial-value problem
loss assessment
loss model
Impact response of low-density foam impinging onto viscoelastic bar: A theoretical analysis
期刊论文
COMPOSITE STRUCTURES, 2018, 卷号: 200, 页码: 47-58
作者:
Liu, Hu
;
Yang, Jialing
;
Liu, Hua
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Low-density foam
Dynamic response
Impact
Viscoelastic bar
Shock wave
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