Influences of meridional flowpath on the performance of swept blade in an axial compressor stage

被引：0
|
作者：
Yu, Xian-Jun [1 ,2 ,3 ]
Xu, Peng-Fei [1 ]
Zhang, Yi-Fei [1 ]
Liu, Bao-Jie [2 ,3 ]
机构：
[1] School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, China
[2] National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, China
[3] Collaborative Innovation Center for Advanced Aero-Engine, Beijing,100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2015年 / 30卷 / 08期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I：
10.13224/j.cnki.jasp.2015.08.011
中图分类号：
学科分类号：
摘要：
Compressors - Axial flow turbomachinery
引用
收藏
页码：1875 / 1887
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