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Numerical Study of Improving Aerodynamic Performance of Low Solidity LPT Cascade through Increasing Trailing Edge Thickness

LI Chao YAN Peigang WANG Xiangfeng HAN Wanjin WANG Qingchao

热科学学报（英文版）2016，Vol.25Issue(4)：342-348,7.

热科学学报（英文版）2016，Vol.25Issue(4)：342-348,7.DOI:10.1007/s11630-016-0869-4

Numerical Study of Improving Aerodynamic Performance of Low Solidity LPT Cascade through Increasing Trailing Edge Thickness

LI Chao ¹YAN Peigang ¹WANG Xiangfeng ¹HAN Wanjin ¹WANG Qingchao¹

作者信息

1. School of Energy science and engineering, Harbin Institute of Technology, Harbin 150001, China
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摘要

关键词

Aircraft engine/low pressure turbine/trailing edge thickness/profile loss/flow control

Key words

Aircraft engine/low pressure turbine/trailing edge thickness/profile loss/flow control

引用本文复制引用

LI Chao,YAN Peigang,WANG Xiangfeng,HAN Wanjin,WANG Qingchao..Numerical Study of Improving Aerodynamic Performance of Low Solidity LPT Cascade through Increasing Trailing Edge Thickness[J].热科学学报（英文版）,2016,25(4):342-348,7.

基金项目

This work was supported by the National Foundation for Innovative Research Groups of China (Grant No.51421063). （Grant No.51421063）

热科学学报（英文版）

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ISSN：1003-2169

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