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Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade
期刊论文
Applied Thermal Engineering, 2019, 卷号: 147, 页码: 347-360
作者:
Du, Kun
;
Li, Zhigang
;
Li, Jun
;
Sunden, Bengt
收藏
  |  
浏览/下载:44/0
  |  
提交时间:2019/11/19
Blade tip
First stage turbine blades
High pressure turbine
K-Omega turbulence model
Multi-cavity
Reynolds averaged Navier Stokes (RANS)equations
Threedimensional (3-d)
Turbine inlet temperature
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
收藏
  |  
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
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions
会议论文
Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
作者:
Prapamonthon P
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Zhang MH(张莫晗)
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  |  
浏览/下载:15/0
  |  
提交时间:2020/11/20
Aerothermal condition
Cooling effectiveness
Cooling performance
Thermal sensitivity
Turbine vane
Effects of location and profile of upstream slot on the endwall aerothermal performance of a gas turbine blade
期刊论文
APPLIED THERMAL ENGINEERING, 2018, 卷号: 140, 页码: 637-656
作者:
Song, Liming
;
Zhu, Peiyuan
;
Li, Jun
;
Feng, Zhenping
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  |  
浏览/下载:8/0
  |  
提交时间:2019/11/19
Numerical simulation
Film cooling
Gas turbine
Upstream slot
Blade endwall
Aerothermal performance
Effects of upstream slot geometry on the endwall aerothermal performance of a gas turbine blade under different ejection angle conditions
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 卷号: 115, 页码: 652-669
作者:
Zhu, Peiyuan
;
Song, Liming
;
Li, Jun
;
Feng, Zhenping
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  |  
浏览/下载:2/0
  |  
提交时间:2019/11/26
Slot geometry
Numerical simulation
Endwall heat transfer
Gas turbine blade
Film cooling
Heat Transfer of Winglet Tips in a Transonic Turbine Cascade
期刊论文
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2017
Zhong, Fangpan
;
Zhou, Chao
;
Ma, H.
;
Zhang, Q.
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  |  
浏览/下载:5/0
  |  
提交时间:2017/12/03
AEROTHERMAL PERFORMANCE
TRANSFER COEFFICIENTS
BLADE TIPS
SQUEALER
GEOMETRY
CLEARANCE
LEAKAGE
REGIONS
FLOW
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings
会议论文
Xiamen, China, 6-9 March 2017
作者:
Li GL(李广利)
;
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ(徐应洲)
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  |  
浏览/下载:25/0
  |  
提交时间:2018/01/16
Aerodynamics
Angle Of Attack
Angle Of Attack Indicators
Boundary Layers
Drag
Drag Coefficient
High Pressure Effects
Hypersonic Aerodynamics
Hypersonic Flow
Spacecraft
NUMERICAL INVESTIGATION OF THE BLADE TIP AND OVERTIP CASING AEROTHERMAL PERFORMANCE IN A HIGH PRESSURE TURBINE STAGE
会议论文
作者:
Du, Kun
;
Li, Zhigang
;
Li, Jun
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/02
Numerical Investigation of the Blade Tip and Overtip Casing Aerothermal Performance in a High Pressure Turbine Stage
会议论文
作者:
Kun Du, Zhigang Li, and Jun Li
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  |  
浏览/下载:9/0
  |  
提交时间:2017/07/20
Effects of tip cavity geometries on the aerothermal performance of the transonic turbine blade with cavity tip
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2016, 卷号: 230, 页码: 319-331
作者:
Li, Jun
;
Du, Kun
;
Song, Liming
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  |  
浏览/下载:11/0
  |  
提交时间:2019/11/26
aerothermal performance
numerical simulation
Transonic turbine blade
cavity tip
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