首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Influence of coupled boundary layer suction and bowed blade on flow field and performance of a diffusion cascade
Authors:Cao Zhiyuan  Liu Bo  Zhang Ting  Yang Xiqiong  Chen Pingping
Institution:1. College of Engineering, Peking University, Beijing 100871, China;2. School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;3. AECC Xi'an Aero-engine Controls Co., LTD, Xi'an 710077, China
Abstract:Based on the investigation of mid-span local boundary layer suction and positive bowed cascade, a coupled local tailored boundary layer suction and positive bowed blade method is devel-oped to improve the performance of a highly loaded diffusion cascade with less suction slot. The effectiveness of the coupled method under different inlet boundary layers is also investigated. Results show that mid-span local boundary layer suction can effectively remove trailing edge sep-aration, but deteriorate the flow fields near the endwall. The positive bowed cascade is beneficial for reducing open corner separation, but is detrimental to mid-span flow fields. The coupled method can further improve the performance and flow field of the cascade. The mid-span trailing edge sep-aration and open corner separation are eliminated. Compared with linear cascade with suction, the coupled method reduces overall loss of the cascade by 31.4%at most. The mid-span loss of the cas-cade decreases as the suction coefficient increases, but increases as bow angle increases. The endwall loss increases as the suction coefficient increases. By contrast, the endwall loss decreases signifi-cantly as the bow angle increases. The endwall loss of coupled controlled cascade is higher than that of bowed cascade with the same bow angle because of the spanwise inverse'C"shaped static pres-sure distribution. Under different inlet boundary layer conditions, the coupled method can also improve the cascade effectively.
Keywords:Axial compressor  Boundary layer suction  Bowed blade  Corner separation  Coupled method  Passage vortex
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号