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Effect of Winglet Geometry Arrangement and Incidence on Tip Clearance Control in a Compressor Cascade

HAN Shaobing ZHONG Jingjun LU Huawei KAN Xiaoxu YANG Ling

热科学学报（英文版）2014，Vol.23Issue(4)：381-390,10.

热科学学报（英文版）2014，Vol.23Issue(4)：381-390,10.DOI:10.1007/s11630-014-0721-7

Effect of Winglet Geometry Arrangement and Incidence on Tip Clearance Control in a Compressor Cascade

HAN Shaobing ¹ZHONG Jingjun ¹LU Huawei ¹KAN Xiaoxu ¹YANG Ling¹

作者信息

1. Marine Engineering College, Dalian Maritime University, Dalian 116026, China
折叠

摘要

关键词

blade tip winglet/ compressor cascade/ incidence/ tip clearance flow

Key words

blade tip winglet/ compressor cascade/ incidence/ tip clearance flow

引用本文复制引用

HAN Shaobing,ZHONG Jingjun,LU Huawei,KAN Xiaoxu,YANG Ling..Effect of Winglet Geometry Arrangement and Incidence on Tip Clearance Control in a Compressor Cascade[J].热科学学报（英文版）,2014,23(4):381-390,10.

基金项目

supported by the National Natural Science Foundation of China (No.51076018) （No.51076018）

the Fundamental Research Funds for the Central Universities(No.3132014041) （No.3132014041）

and Specialized Research Fund for the Doctoral Program of Higher Education. （）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

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