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：

引用