Effect of Winglet Geometry Arrangement and Incidence on Tip Clearance Control in a Compressor Cascade
- ISSN号:1003-2169
- 期刊名称:《热科学学报:英文版》
- 时间:0
- 分类:V231.3[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术] TU473.1[建筑科学—结构工程;建筑科学—土工工程]
- 作者机构:Marine Engineering College, Dalian Maritime University, Dalian 116026, China
- 相关基金:supported by the National Natural Science Foundation of China (No.51076018); the Fundamental Research Funds for the Central Universities(No. 3132014041); and Specialized Research Fund for the Doctoral Program of Higher Education.
关键词:
叶尖泄漏涡, 压气机叶栅, 几何布置, 发病率, 间隙控制, 翼梢小翼, 压力损失系数, 非设计条件, blade tip winglet, compressor cascade, incidence, tip clearance flow
中文摘要:
ZHONG Jingjun: Professor