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

弯曲壁面上离散孔气膜冷却均匀性的实验研究
引用本文:姚永庆,夏彬,葛绍岩,邹福康.弯曲壁面上离散孔气膜冷却均匀性的实验研究[J].航空动力学报,1988,3(2):161-163,190.
作者姓名:姚永庆  夏彬  葛绍岩  邹福康
作者单位:中国科学院工程热物理研究所 (姚永庆,夏彬,葛绍岩),美国德克赛尔大学(邹福康)
摘    要:本文利用传质比拟传热的方法,研究离散孔气膜冷却在整个弯曲壁面上沿与主流垂直方向的冷却均匀性。比较了单、双排孔和前、后排孔流量不等时,在不同吹风比的条件下,在凸、凹表面上冷却均匀性的特征。

收稿时间:1986/10/1 0:00:00

EXPERIMENTAL INVESTIGATION ON FILM-COOLING UNIFORMITY OF DISCRETE HOLES OVER A CURVED SURFACE
Yao Yongqing,Xia Bin,Ge Shaoyen.EXPERIMENTAL INVESTIGATION ON FILM-COOLING UNIFORMITY OF DISCRETE HOLES OVER A CURVED SURFACE[J].Journal of Aerospace Power,1988,3(2):161-163,190.
Authors:Yao Yongqing  Xia Bin  Ge Shaoyen
Institution:Institute of Engineering ThermoPhysics;Institute of Engineering ThermoPhysics;Institute of Engineering ThermoPhysics
Abstract:The film-cooling uniformity of discrete holes in the direction normal to main stream is investigated by means of heat and mass analogy. At different blowing ratios, the features of the film-cooling uniformity for one row and two rows of discrete holes are compared. It is found that the film-cooling uniformity on the concave surface is better than that on the convex one.
Keywords:
本文献已被 CNKI 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