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

基于耗散函数的低速扩压叶栅损失机理探讨
引用本文:刘华坪,陈焕龙,杨晓光,陈浮.基于耗散函数的低速扩压叶栅损失机理探讨[J].航空动力学报,2011,26(2):289-296.
作者姓名:刘华坪  陈焕龙  杨晓光  陈浮
作者单位:哈尔滨工业大学,能源科学与工程学院,推进理论与技术研究所,哈尔滨,150001
摘    要:推导了含耗散函数项的总压输运方程,利用总压损失,熵增,耗散函数等参数分析某扩压叶栅流动与损失特性,探讨其损失产生机理.研究表明:栅内损失主要来源于叶片前缘附近、流道表面、尾迹区、分离区与主流交界区的流动耗散;分离区仅是高总压损失和高熵值的低能流体聚集区,而非高损失来源区;通过减小分离区以提高叶栅件能的控制方法本质是通过...

关 键 词:扩压叶栅  流动分离  损失来源  熵增  耗散函数
收稿时间:2009/12/18 0:00:00
修稿时间:2010/3/30 0:00:00

Study of loss mechanism in low speed compressor cascade using dissipation function
LIU Hua-ping,CHEN Huan-long,YANG Xiao-guang and CHEN Fu.Study of loss mechanism in low speed compressor cascade using dissipation function[J].Journal of Aerospace Power,2011,26(2):289-296.
Authors:LIU Hua-ping  CHEN Huan-long  YANG Xiao-guang and CHEN Fu
Institution:LIU Hua-ping,CHEN Huan-long,YANG Xiao-guang,CHEN Fu(Institute of Propulsion Theory and Technology,School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China)
Abstract:The transport equation of total pressure containing dissipation functi on was derived.Through experimental and numerical studies of a low speed compres sor cascade,the characteristics of flow and loss distribution were discussed in detail,then the loss mechanism was obtained.The results show that:the high casca de loss originates from dissipation in the area near the blade leading edge,blad e and end wall surface,wakes,as well as the area between the separation and main stream.Moreover,the separation zone i...
Keywords:compressor cascade  flow separation  loss source  entropy increase  
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