Effects of Cropped Blade Tip Leading Edge on Aerodynamic Performance of Transonic Compressor

被引：0
|
作者：
Qin, Li-Tao [1 ]
Zhang, Hai-Deng [1 ]
Zhou, Liu-Cheng [1 ]
He, Wei-Feng [1 ]
Wu, Yun [1 ]
Li, Ying-Hong [1 ]
机构：
[1] Science and Technology on Plasma Dynamics Laboratory, Aeronautics Engineering College, Air Force Engineering University, Xi’an,710038, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2022年 / 43卷 / 10期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I：
210346
中图分类号：
学科分类号：
摘要：
Aerodynamic stalling - Compressors - Deterioration - Efficiency - Mass transfer - Numerical methods - Transonic flow
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