8   Artículos

 
en línea
Dongjie Yan, Hongmei Jiang, Jieling Li, Wenbo Xie, Zhaoguang Wang, Shaopeng Lu and Qiang Zhang    
In high-pressure turbines, there is a large difference in temperature between the mainstream and the turbine blade surface. Most of the turbine blade tip heat transfer studies were conducted under the assumption that the Over-Tip-Leakage (OTL) flow field... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Hongmei Jiang, Xu Peng, Wenbo Xie, Shaopeng Lu and Yongmin Gu    
The high-speed Over-Tip-Leakage (OTL) flow has a significant impact on the aerodynamic performance of the High-Pressure Turbine (HPT) passage and generates high thermal load for the blade tip. Different tip sealing and cooling design strategies are appli... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Song Xue and Wing F. Ng    
This article provides an overview of gas turbine blade tip external cooling technologies. It is not the intention to comprehensively review all the publications from past to present. Instead, selected reports, which represent the most recent progress in ... ver más
Revista: Aerospace    Formato: Electrónico

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