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

应用嵌入式H型网格技术计算孤立翼型绕流场
引用本文:张谋进,黄灿明.应用嵌入式H型网格技术计算孤立翼型绕流场[J].航空动力学报,2001,16(2):128-130,127.
作者姓名:张谋进  黄灿明
作者单位:1.西安交通大学,陕西西安710089
摘    要:提出一种嵌入式H型网格技术,用于生成孤立翼型和叶栅的计算网格。与传统的H型网格相比,采用嵌入式H型网格时,翼型头部及尾部附近的网格畸变很容易得到控制,有益于提高计算的准确性。 

关 键 词:嵌入式网格    翼型    N-S方程
文章编号:1000-8055(2001)02-0128-03
收稿时间:2000/6/23 0:00:00
修稿时间:2000年6月23日

Computation of Flow around Isolated Airfoils with Embedded H-Grid
ZHANG Mou jin and Wong C M.Computation of Flow around Isolated Airfoils with Embedded H-Grid[J].Journal of Aerospace Power,2001,16(2):128-130,127.
Authors:ZHANG Mou jin and Wong C M
Institution:1.Institute of Fluid Machinery,Xi′an Jiaotong University,Xi′an710089,China2.Dept.of Mechanical Engineering,The Hong Kong Polytechnic University,Hong Kong,China
Abstract:An embedded H grid technique is employed for generating grids of isolated airfoils and cascades.Comparing with original H grid,the embedded H grid is easy to control the orthogonality of grids around the leading and trailing edges of airfoils and useful to improving the accuracy of computation.Two numerical analyses of isolated airfoils under different incidences show that the results of computation using the embedded H grid are in good agreement with experimental data.
Keywords:embedded grider  airfoils  Navier  Stokes equation
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