附面层抽吸对高负荷压气机叶栅流场的影响  

Effects of boundary layer suction on the flow fields of highly-loaded compressor cascades

作　　者：陈绍文 郭爽[2] 宋宇飞[2] 陈浮[2] 刘顺隆[1] 

机构地区：[1]哈尔滨工程大学动力与能源工程学院,黑龙江哈尔滨150001 [2]哈尔滨工业大学能源科学与工程学院,黑龙江哈尔滨150001

出　　处：《推进技术》2009年第5期588-593,共6页Journal of Propulsion Technology

基　　金：国家自然科学基金(50646021);国家科技部"九七三"项目资助(2007CB210100)

摘　　要：在低速条件下,对不同吸气位置和吸气量的高负荷吸附压气机叶栅流场进行了实验研究,分析了吸气位置和吸气量对高负荷压气机叶栅流场的影响。结果表明,吸气位置和吸气量对高负荷吸气压气机叶栅流场影响显著,且在小吸气量下流场就有明显改善;附面层抽吸有效减小了积聚在吸力面角区的低能流体,流动分离被抑制,总损失下降明显,且抽吸对叶栅流场的影响随吸气量的增加而逐渐增大;在吸力面后部流动充分发展区域,采用附面层抽吸对抑制流动分离具有更好的效果。The detailed experimental investigations into highly loaded aspirated compressor cascade with different suction locations and suction flow rates are carried out in low-speed conditions.The effects of suction location and suction flow rate on flow fields of highly loaded aspirated compressor cascade are analyzed.The results show that suction slot location and suction flow rate have pronounced effects on the flow fields of the highly-loaded compressor cascades.The improvement of flow fields is notable at lowe...

关 键 词：压气机 叶栅 边界层抽吸+ 流动分布 

分 类 号：V231.3[航空宇航科学与技术—航空宇航推进理论与工程]