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Investigation of the Impact of Relative Position on Corner Stall in Tandem Stators

  • Chuanhai Zhang
  • , Baojie Liu
  • , Diyun Chen
  • , Zhuyu Jiang
  • , Shaoyuan Yue*
  • *此作品的通讯作者
  • China Aerodynamics Research and Development Center

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This study employs numerical simulations to investigate the impact of pitch relative positions (PP) and axial relative positions (AO) on tandem stator performance and corner stall. The results indicate that two distinct types of corner stall behavior are exhibited. With PP values of 0.50 and 0.60, the rear blade stalls first, while with values of 0.70 to 0.90, it is the front blade that stalls first. Additionally, there is a trend for corner stall to be delayed as PP value increases, which is attributed to PP changing the load distribution between front and rear blades. Corner stall is also delayed as AO increases. The mechanism is that the adverse pressure gradient of the suction surface boundary layer in the root regions decreases with AO increasing, which delays boundary layer separation. Investigations into tandem stators with various combinations of PP and AO show that the type of corner stall primarily correlates with changes of PP, and type of front blade corner stall first associates with wider operating range and lower losses. Considering both loss and stall margin, the optimal PP range for the tandem stator root is between 0.80 and 0.90, while the optimal AO range is between −0.05 and 0.

源语言英语
主期刊名Proceedings of the 2nd Aerospace Frontiers Conference, AFC 2025 - Volume VI
出版商Springer Science and Business Media Deutschland GmbH
112-131
页数20
ISBN(印刷版)9789819530366
DOI
出版状态已出版 - 2026
活动2nd Aerospace Frontiers Conference, AFC 2025 - Beijing, 中国
期限: 11 4月 202514 4月 2025

出版系列

姓名Lecture Notes in Mechanical Engineering
ISSN(印刷版)2195-4356
ISSN(电子版)2195-4364

会议

会议2nd Aerospace Frontiers Conference, AFC 2025
国家/地区中国
Beijing
时期11/04/2514/04/25

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