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科研机构
北京航空航天大学 [55]
内容类型
期刊论文 [42]
会议论文 [13]
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2020 [1]
2019 [12]
2018 [10]
2017 [10]
2016 [3]
2015 [3]
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专题:北京航空航天大学
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Effect of film hole geometry and blowing ratio on film cooling performance
期刊论文
Applied Thermal Engineering, 2020, 卷号: 165
作者:
Cao, Nan
;
Li, Xue
;
Wu, Zeyu
;
Luo, Xiang
收藏
  |  
浏览/下载:32/0
  |  
提交时间:2019/12/30
A study for the film cooling performance on the turbine blade suction side tip region under rotating conditions
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 138, 页码: 483-495
作者:
Wang, Haichao
;
Tao, Zhi
;
Zhou, Zhiyu
;
Zhou, Huimin
;
Ma, Yiwen
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Experimental and numerical study of the film cooling performance of the suction side of a turbine blade under the rotating condition
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 136, 页码: 436-448
作者:
Wang, Haichao
;
Tao, Zhi
;
Zhou, Zhiyu
;
Han, Feng
;
Li, Haiwang
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2019/12/30
Reynolds number
Turbine components
Turbomachine blades
Vortex flow
Blowing ratio
Cooling effectiveness
Experimental and numerical studies
Film cooling performance
Passage vortex
Rotating conditions
Rotational effects
Turbine blade
Cooling
Thermal state calculation of chamber in small thrust liquid rocket engine for steady state pulsed mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 页码: 253-262
作者:
Vorobyev, Alexey Gennadievich
;
Vorobyeva, Svatlana Sergeevna
;
Zhang, Lihui
;
Beliaev, Evgeniy Nikolaevich
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2019/12/30
Combustion chamber
Film cooling
Mathematical model
Nonstationary thermal mode
Small thrust liquid rocket engine
Steady pulse mode
Thermal state
Experimental investigation on the effects of rotation and the blowing ratio on the leading-edge film cooling of a twist turbine blade
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 129, 页码: 47-58
作者:
Li, Hai-wang
;
Han, Feng
;
Ma, Yi-wen
;
Wang, Hai-chao
;
Zhou, Zhi-yu
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Film cooling
Leading edge
Rotating blade
Effectiveness
Blowing ratio
Film cooling and aerodynamic performances of a turbine nozzle guide vane with trenched cooling holes
期刊论文
APPLIED THERMAL ENGINEERING, 2019, 卷号: 150, 页码: 150-163
作者:
He, Wei
;
Deng, Qinghua
;
Zhou, Weilun
;
Gao, Tieyu
;
Feng, Zhenping
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Trenched cooling holes
Turbine vane
Adiabatic film cooling effectiveness
Discharge coefficient
Total pressure loss
An investigation for the turbine blade film cooling performance on the suction side tip region under rotating condition
期刊论文
Applied Thermal Engineering, 2019, 卷号: 150, 页码: 864-874
作者:
Wang, H.
;
Tao, Z.
;
Zhou, Z.
;
Zhao, G.
;
Han, F.
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Cooling
Numerical models
Reynolds number
Turbines
Turbomachine blades
Film cooling performance
Film performance
K epsilon models
Leakage vortex
Rotating blades
Rotating conditions
Rotating turbines
Rotation effect
Vortex flow
Numerical investigation about backflow of film cooling in static turbine blade leading edge
期刊论文
ADVANCES IN MECHANICAL ENGINEERING, 2019, 卷号: 11
作者:
Gao, Chao
;
Li, Haiwang
;
Zhou, Huimin
;
Ma, Yiwen
;
You, Ruquan
收藏
  |  
浏览/下载:9/0
  |  
提交时间:2019/12/30
Numerical simulation
turbine blade
leading edge
film cooling
backflow
Transient simulation of pulsed purge film cooling on flow and thermal characteristics of a turbine endwall
期刊论文
APPLIED THERMAL ENGINEERING, 2019, 卷号: 161
作者:
Liu, Youhong
;
Luo, Yifu
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Pulsed purge flow
Film cooling
Turbine endwall
Numerical simulation
Film cooling of cylindrical holes on turbine blade suction side near leading edge
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 141, 页码: 669-679
作者:
Zhou, Zhiyu
;
Li, Haiwang
;
Wang, Haichao
;
Xie, Gang
;
You, Ruquan
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Film cooling
Turbine blade
Rotation
Blowing ratio
Reynolds number
Injection angle
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