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:
Experiment on influences of inlet temperature and pressure on vortex tube's performance
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所属单位:能源与动力学院
发表刊物:Hangkong Dongli Xuebao
摘要:Experiments were carried out to study the influences of the inlet/outlet expansion ratio (2~5), the throttle setting value (1~11) and the inlet temperature (313~373K) on vortex tube's performance. The variation of refrigeration and heating effects was obtained along with above parameters. It was found in experiments that the performance of vortex tube was enhanced with the increasing inlet expansion ratio, promoting the in-tube vortex intensity and increasing inlet the angular velocity gradient at different radiuses. The refrigeration effect increased by 10.9% and heating effect increased by 46.5% separately. With the rise of throttle setting value, the degree of energy exchange between the cold/heating flow increased, the eddy effect strengthened and cold flow rate increased by 47.3%. The performance of the vortex tube was improved with the increase of the inlet temperature. All the results show that as the inlet temperature increases by every 20K, the refrigeration effect at the cold side is enhanced by about 12%, while the heating effect at hot side is improved by about 5%. © 2017, Editorial Department of Journal of Aerospace Power. All right reserved.
ISSN号:1000-8055
是否译文:否
发表时间:2017-03-01
合写作者:Gong, Di-Lan,Deng, Ming,Yan, Ben,Wang, Peng-Fei,Zeng, Jun
通讯作者:毛军逵