个人信息Personal Information
教授 博士生导师
招生学科专业:
动力工程及工程热物理 -- 【招收博士、硕士研究生】 -- 能源与动力学院
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
主要任职:江苏省“航空动力系统”重点实验室主任
其他任职:《航空发动机》副主编、《航空学报》中英文版编委、《推进技术》编委
毕业院校:南京航空航天大学
学历:南京航空航天大学
学位:工学博士学位
所在单位:能源与动力学院
办公地点:明故宫校区A10楼519房间、435房间
联系方式:mjkpe@nuaa.edu.cn
电子邮箱:
Numerical Study of Suspending Tube Heat Transfer Unit for a Blade Tip Clearance Control System
点击次数:
所属单位:能源与动力学院
发表刊物:Tuijin Jishu
摘要:To improve the effects of cross-flow and the usage of coolant heat sinks, the numerical simulation is carried out in the present study for a typical heat transfer unit in a new type of suspending tube cooling structure of a blade tip clearance control system. The effects of some key parameters are studied on the heat transfer characteristics of the cooling structure, such as the impinging Reynolds number, distance of jet to jet and outflow type. It is found that a phenomenon of 'fountain flow' appears formed by the interaction of adjacent impinging jets of suspending tubes. With decreasing the impinging Reynolds number and increasing the distance of jet to jet, the heat transfer on the target is weakened and the phenomenon of 'fountain flow' is no more significant. Due to the space limitation caused by the suspending tubes and the cover plate, the circumferential and axial cross-flows are formed in impinging chamber. When the coolant flow exits from the side of the case, the axial cross-flow is most significant on the casing surface. Compared to the outflow from the side of the case, the heat transfer between the two high ribs is enhanced considerably when the outflow is from the top of the case, or from both the top and the side of the case. A maximum increase is up to around 20% when the outflow is from the top. © 2019, Editorial Department of Journal of Propulsion Technology. All right reserved.
ISSN号:1001-4055
是否译文:否
发表时间:2019-02-01
合写作者:Zhang, Yang,Liu, Yuan-Jian,Li, Rui,李睿华,Liu, Zhao-Ying
通讯作者:Zhang, Yang,毛军逵