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Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield

LIU Jun DU Qiang LIU Guang WANG Pei ZHU Junqiang

热科学学报（英文版）2014，Vol.23Issue(5)：494-504,11.

热科学学报（英文版）2014，Vol.23Issue(5)：494-504,11.DOI:10.1007/s11630-014-0734-2

Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield

LIU Jun ¹DU Qiang ¹LIU Guang ¹WANG Pei ¹ZHU Junqiang¹

作者信息

1. Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
折叠

摘要

关键词

Intermediate Turbine Duct/ Integrated Design Concept/ Flowfield Analysis/ Total Pressure Loss Analysis

Key words

Intermediate Turbine Duct/ Integrated Design Concept/ Flowfield Analysis/ Total Pressure Loss Analysis

引用本文复制引用

LIU Jun,DU Qiang,LIU Guang,WANG Pei,ZHU Junqiang..Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield[J].热科学学报（英文版）,2014,23(5):494-504,11.

基金项目

This work is supported by grants from the National Natural Science Foundation of China (No.51306177). （No.51306177）

热科学学报（英文版）

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ISSN：1003-2169

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