Mechanism of Effects of Rotor Blade Tip Jet Slot on Performance and Flow Structure of Transonic Axial Compressor

被引：0
|
作者：
Gao, Tian-Yi [1 ]
Zhang, Guo-Chen [1 ]
Xu, Zhi-Hui [1 ]
Liu, Peng-Cheng [1 ]
机构：
[1] Key Laboratory of Advanced Measurement and Test Technique for Aviation Propulsion System, Liaoning Province, School of Aero-engine, Shenyang Aerospace University, Shenyang,110136, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2022年 / 43卷 / 03期
关键词：
Blade tip - Performance - Rotor blades - Rotor slots - Slot position - Stability margins - Tip jet - Total pressure ratio - Trailing edges - Transonic axial compressors;
D O I：
200405
中图分类号：
学科分类号：
摘要：
20
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