首页 | 本学科首页   官方微博 | 高级检索  
     

结冰计算中翼面网格重构研究
引用本文:孙志国,朱程香,付斌,朱春玲. 结冰计算中翼面网格重构研究[J]. 航空学报, 2011, 32(2): 231-241. DOI: CNKI:11-1929/V.20101111.0915.030
作者姓名:孙志国  朱程香  付斌  朱春玲
作者单位:南京航空航天大学航空宇航学院,江苏南京,210016
摘    要:对结冰数值计算中的网格生成进行了深入研究,针对结冰后几何边界的复杂性及边界依赖于时间步长变化对网格生成的影响展开了分析.网格生成是结冰计算的基础,文中基于求解椭圆形偏微分方程(PDEs)生成了未结冰时翼面周围的背景网格,采用Hilgenstock源项构造方法,合理控制了结冰边界周围的网格间距和正交性.模型表面结冰后,为...

关 键 词:结冰代码  网格重构  贴体网格  控制源项  网格分区  机翼

Research of Grid Reconstruction on Wing Surfaces for Icing Calculation
SUN Zhiguo,ZHU Chengxiang,FU Bin,ZHU Chunling. Research of Grid Reconstruction on Wing Surfaces for Icing Calculation[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(2): 231-241. DOI: CNKI:11-1929/V.20101111.0915.030
Authors:SUN Zhiguo  ZHU Chengxiang  FU Bin  ZHU Chunling
Affiliation:College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Abstract:This article studies grid generation for the calculation of airfoil ice accretion; in particular, it analyzes how to deal with the effect brought by geometrically complex and time-dependent leading edge accretion. As the first step of icing calculation, a grid is generated by solving the elliptic partial differential equations(PDEs). The forcing terms are automatically chosen in the manner of Hilgenstock method such that orthogonality and spacing control on the icing smoothed boundary are achieved. In order to improve the efficiency, quality and reliability of grids, two partition ideas and grid reconstruction methods are introduced and validated simultaneously. Finally, validation of the usefulness of the method developed is completed on two and three dimensional airfoils using the NUAA-ICE3D software, which has integrated the grid modules.
Keywords:ice accretion code  grid reconstruction  body-fitted grid  forcing function terms  grid partition  aifoils
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载全文
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