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

Helmholzt振荡腔对光滑圆管换热的强化实验
引用本文:丁水汀,高翔宇,邓宏武,徐国强,陶智,邹正平.Helmholzt振荡腔对光滑圆管换热的强化实验[J].航空动力学报,2007,22(2):199-204.
作者姓名:丁水汀  高翔宇  邓宏武  徐国强  陶智  邹正平
作者单位:北京航空航天大学,能源与动力工程学院航空发动机气动热力重点实验室,北京,100083;北京航空航天大学,能源与动力工程学院航空发动机气动热力重点实验室,北京,100083;北京航空航天大学,能源与动力工程学院航空发动机气动热力重点实验室,北京,100083;北京航空航天大学,能源与动力工程学院航空发动机气动热力重点实验室,北京,100083;北京航空航天大学,能源与动力工程学院航空发动机气动热力重点实验室,北京,100083;北京航空航天大学,能源与动力工程学院航空发动机气动热力重点实验室,北京,100083
摘    要:气流通过Helmholzt振荡腔产生脉动气流.实验固定振荡腔进出口直径和振荡腔直径, 在改变振荡腔腔长的情况下, 在圆管进口Re为22000到82000范围内对等热流加热条件下的圆管换热实验进行了研究.实验将脉动气流所产生的圆管换热效果与定常气流产生的换热效果进行对比.结果表明:气流流经Helmholzt振荡腔后对圆管换热有强化作用, 其强化作用主要集中在沿圆管轴向前10倍直径的长度上, 强化比约为1.1-1.9.随着距离增大换热强化比迅速减小.振荡腔腔长对换热效果有较强的影响. 

关 键 词:航空、航天推进系统  Helmholzt  脉动气流  圆管对流换热
文章编号:1000-8055(2007)02-0199-06
收稿时间:2006/1/20 0:00:00
修稿时间:2006年1月20日

An experimental study of the effects of air flow through Helmholzt cavity on heat transfer within a smooth round tube
DING Shui-ting,GAO Xiang-yu,DENG Hong-wu,XU Guo-qiang,TAO Zhi and ZHOU Zheng-ping.An experimental study of the effects of air flow through Helmholzt cavity on heat transfer within a smooth round tube[J].Journal of Aerospace Power,2007,22(2):199-204.
Authors:DING Shui-ting  GAO Xiang-yu  DENG Hong-wu  XU Guo-qiang  TAO Zhi and ZHOU Zheng-ping
Institution:National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:When the air flows through the Helmholzt oscillation cavity,it will be pulsing.The inlet and outlet diameters of Helmholzt cavity remain const,but the length of cavity is changed so that,the Reynolds number at the inlet changes from 22 000 to 82 000.The experimental investigation was conducted under equiflux conditions.Comparison was made between the heat transfer coefficient of steady air flow and unsteady air flow.The results show that: The pulse air flow can increase the heat transfer,but the enhancement of heat transfer takes place mainly at the distance of 10 times of the diameter along the axial direction of the round tube.The ratio of enhancement lies between 1.1 to 1.9.This ratio decreaser significantly as the distance becomes longer.Beyond the distance of 10 times of the diameter,the ratio of enhancement fluctuates slightly as the Reynolds number increases.The experimeotal investigation also shows that the heat conduction coefficient is influenced by the length of the Helmholzt cavity.
Keywords:aerospace propulsion system  Helmholzt  pulse air flow  heat conduction of round tube
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
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