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典型层板冷却结构中流体流阻与换热特性的实验
引用本文:陶智,魏豪杰,丁水汀,邓宏武,徐国强,林宇震.典型层板冷却结构中流体流阻与换热特性的实验[J].航空动力学报,2007,22(2):193-198.
作者姓名:陶智  魏豪杰  丁水汀  邓宏武  徐国强  林宇震
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国防重点实验室,北京,100083
基金项目:教育部跨世纪优秀人才培养计划
摘    要:对进气孔、扰流柱和出气孔个数之比为1∶4∶1的典型层板冷却结构的流体流阻与换热特性进行了实验研究.结果表明,对于进、出气板间距不大的层板模型,出气板内表面的换热系数最大,扰流柱表面的换热系数次之,进气板内表面的换热系数最小.对不同层板模型的比较表明,相同流量下随着进气孔直径的增大,流阻系数增大,进气板内表面的换热系数变化不大、出气板内表面的换热减弱;随着出气孔直径的增大,流阻明显减小,进气板内表面的换热减弱,出气板内表面的换热变化不大;随着出气孔倾角的增大,流阻增大,进气板内表面的换热增强,出气板内表面的换热变化不大.

关 键 词:航空、航天推进系统  燃气轮机  层板叶片  对流换热  流阻  层板  冷却结构  流体流  换热特性  实验  models  typical  heat  transfer  characteristics  flow  resistance  investigation  热增强  倾角  热变化  流阻系数  直径  流量  比较  最小  内表面  换热系数
文章编号:1000-8055(2007)02-0193-06
收稿时间:2006/1/17 0:00:00
修稿时间:2006年1月17日

Experimental investigation of flow resistance and heat transfer characteristics of typical lamilloy models
TAO Zhi,WEI Hao-jie,DING Shui-ting,DENG Hong-wu,XU Guo qiang and LIN Yu-zhen.Experimental investigation of flow resistance and heat transfer characteristics of typical lamilloy models[J].Journal of Aerospace Power,2007,22(2):193-198.
Authors:TAO Zhi  WEI Hao-jie  DING Shui-ting  DENG Hong-wu  XU Guo qiang and LIN Yu-zhen
Institution:National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:Experimental investigation of flow resistance and heat transfer characteristics has been carried out on a typical lamilloy model whose ratio of inlet hole,pin-fin,and outlet hole is 1:4:1.The results show that for a lamilloy model,the heat transfer coefficient of the internal surface of outlet board is the highest,followed by the pin-fin's surface,and that of the internal surface of inlet board is the lowest.The comparisons show that at the same mass flow,the flow resistance increases,the heat transfer coefficient of the outlet board decreases,and the heat transfer coefficient of the intlet board changes little by enlarging the inlet hole.Comparisons also show that the flow resistance and the heat transfer coefficient of the inlet board increase,but the heat transfer coefficient of the outlet board has little change by reducing the outlet hole or increasing the obliquity of the outlet hole.
Keywords:aerospace propulsion system  gas turbines  lamilloy blade  heat transfer  flow resistance
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