首页|期刊导航|热科学学报（英文版）|Experimental Investigation of Effects of Suction-Side Squealer Tip Geometry on the Flow Field in a Large-scale Axial Compressor using SPIV

Experimental Investigation of Effects of Suction-Side Squealer Tip Geometry on the Flow Field in a Large-scale Axial Compressor using SPIV

MA Hongwei WEI Wei WANG Lixiang TIAN Yangtao

热科学学报（英文版）2015，Vol.24Issue(4)：303-312,10.

热科学学报（英文版）2015，Vol.24Issue(4)：303-312,10.DOI:10.1007/s11630-015-0789-8

Experimental Investigation of Effects of Suction-Side Squealer Tip Geometry on the Flow Field in a Large-scale Axial Compressor using SPIV

MA Hongwei ¹WEI Wei ²WANG Lixiang ³TIAN Yangtao⁴

作者信息

1. Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,
2. School of Energy and Power Engineering,Beihang University,Beijing,100191,China
3. Collaborative Innovation Center of Advanced Aero-Engine,Beijing,100191,China
折叠

摘要

关键词

tip leakage vortex/suction side squealer/axial compressor/SPIV/instantaneous flow field

Key words

tip leakage vortex/suction side squealer/axial compressor/SPIV/instantaneous flow field

引用本文复制引用

MA Hongwei,WEI Wei,WANG Lixiang,TIAN Yangtao..Experimental Investigation of Effects of Suction-Side Squealer Tip Geometry on the Flow Field in a Large-scale Axial Compressor using SPIV[J].热科学学报（英文版）,2015,24(4):303-312,10.

基金项目

This study was co-supported by the National Natural Science Foundation of China (Grant No.51161130525/No.51136003),the 111 Project (No.B07009) This study was co-supported by the National Natural Science Foundation of China (Grant No.51161130525/ No.51136003),the 111 Project (No.B07009),and the Innovation Foundation of BUAA for PhD Graduates (No.YWF-14-YJSY-014). （Grant No.51161130525/No.51136003）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

访问量0

下载量0

段落导航