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西安交通大学 [34]
北京航空航天大学 [13]
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Effect of gas turbine endwall misalignment with slashface leakage on the blade endwall aerothermal performance
期刊论文
International Journal of Heat and Mass Transfer, 2019, 卷号: 131, 页码: 1247-1259
作者:
Zhang, Kaiyuan
;
Li, Zhigang
;
Li, Jun
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  |  
浏览/下载:36/0
  |  
提交时间:2019/11/19
Computational results
Cooling effectiveness
End-wall
Film cooling
Heat transfer performance
K-Omega turbulence model
Numerical calculation
Reynolds averaged Navier Stokes (RANS)equations
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
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  |  
浏览/下载:17/0
  |  
提交时间:2019/11/19
Total pressure loss
Turbine vane
Adiabatic film cooling effectiveness
Discharge coefficient
Trenched cooling holes
Influence of streamwise position of crescent-shaped block on flat-plate film cooling characteristics
期刊论文
JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2019, 卷号: 41, 期号: 11
作者:
Zhang, Chao
;
Wang, Zhan
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  |  
浏览/下载:13/0
  |  
提交时间:2019/12/11
Gas turbine
Film cooling
Crescent-shaped block
Streamwise position
Cooling effectiveness
Aerodynamic loss
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
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  |  
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
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
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  |  
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
Effects of spanwise distance and density ratio on the characteristic of double-jet film-cooling
期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 1336-1344
作者:
Yao, Jiaxu
;
Xu, Jin
;
Zhang, Ke
;
Wu, Junmei
;
Lei, Jiang
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浏览/下载:2/0
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提交时间:2019/11/19
Density ratio
Double jets
Film cooling
Film cooling effectiveness
Pressure sensitive paints
Effect of Rib Location on the Heat Transfer and Cooling Characteristics at the Squealer Tip in Turbine Stage
期刊论文
Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2018, 卷号: 52, 页码: 116-124
作者:
Ye, Mingliang
;
Yan, Xin
;
He, Kun
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  |  
浏览/下载:4/0
  |  
提交时间:2019/11/19
Aero-dynamic performance
Cooling characteristics
Film cooling
Film cooling effectiveness
Film-cooling characteristics
Isentropic efficiency
Squealer tip
Turbine stages
Effects of streamwise distance and density ratio on film-cooling effectiveness for double-jet film-cooling on a flat plate
会议论文
作者:
Yao, Jiaxu
;
Lei, Jiang
;
Wu, Junmei
;
Fang, Yu
;
Wright, Lesley M.
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  |  
浏览/下载:8/0
  |  
提交时间:2019/11/19
Compound angle
Density ratio
Film cooling
Film cooling effectiveness
Inclination angles
Operation conditions
Pressure sensitive paints
Streamwise distance
Interaction of Flow and Film Cooling Effectiveness Between Double-Jet Film-Cooling Holes With Various Spanwise Distances
期刊论文
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 卷号: 140
作者:
Yao, Jiaxu
;
Xu, Jin
;
Zhang, Ke
;
Lei, Jiang
;
Wright, Lesley M.
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  |  
浏览/下载:3/0
  |  
提交时间:2019/11/26
antikidney vortex cooling effectiveness
double-jet film-cooling (DJFC)
spanwise distance
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