期刊文献+

一种同位网格上的迎风Galerkin有限元方法 被引量:2

A Co-Located Upwind Scheme-Based Galerkin Finite Element Method
下载PDF
导出
摘要 通过 Green定理将对流项变量从微分算子中分离出来 ,从插值函数入手引入迎风格式 ,是对强对流问题 Galerkin有限元计算中对流项变量的一种新的处理方法。按这种方法采用局部斜迎风格式及速—压同位网格公式 ,构成了一种对高 Reynolds数流体流动数值模拟比较有效的有限元方法。数值试验表明 ,采用该方法能较好地提高计算精度。 Invoking Green's theorem to separate the convection variable from the differiential operator of weighted residual equation is a new strategy of using upwind scheme in Galerkin finite element method. As an example, the locally skewed upwind scheme is proposed. By imple-menting this strategy in conjunction with the equal-order velocity-pressure formulation, the convection-dominated fluid flow can be obtained more accurate simulation in complex geometrics. This paper not only has established this new method, but also has proved its accuracy is rather encouraging by its application to some typical examples and comparisons with other literatures.
作者 王旭 谷传纲
出处 《空军工程大学学报(自然科学版)》 CSCD 2000年第3期19-22,共4页 Journal of Air Force Engineering University(Natural Science Edition)
关键词 有限元方法 微分算子 局部斜迎风格式 同位网格法 数值模拟 finite element method differentiator locally skewed upwind scheme equal-order velocity-pressure formulation numerical simulation
  • 相关文献

参考文献6

  • 1[1] Mizukami A, Hughes T J R. A Petrov-Galerkin Finite Element Method for Convection-Dominated Flows:An Accurate Upwinding Technique for Satisfying the Maximum Principle[J]. Comput Methods Appl Mech Eng, 1985,50:181193.
  • 2[2] Hughes T G, Taylor C. Finite Element Programming of the Navier-Stokes Equations[M]. Swansea,U K: Pineridge Press Limtted, 1980.
  • 3[3] Rice J G, Schnipke R J. A Monotone Streamline Upwind Finite Element Method for Convection-Dominated Flows[J]. Comput Methods Appl Mech Eng, 1985, 48:313327.
  • 4[4] Rice J G, Schnipke R J. An Equal-Order Velocity-Pressure Formulation That Does Not Exhibit Spurious Pressure Modes[J]. Comput Methods Appl Mech Eng, 1986, 58:135149.
  • 5[5] Armaly B F, Durst F, Pereira J C F, et al. Experimental and Theoretical Investigation of Backward-Facing Step Flow[J]. J Fluid Mech, 1983,127:473496.
  • 6[6] Ghia U, Ghia K N, Shin C T. High-Re Solutions for Incompressible Flow Using the Navier-Stokes Equations and a Multi-Grid Method[J]. J Comput phys, 1982, 48:387411.

同被引文献9

  • 1陈汝训.固体火箭发动机设计与研究(下)[M].北京:宇航出版社,1991..
  • 2陈延南.应用流体力学[M].北京:航空工业出版社,2006.
  • 3FAA.Airport Design Advisory Circular[S].AC:150/5300-13.
  • 4Gribben B J,Badcock K J,et al.Numerical study of shock-reflection hysteresis in an under expanded jet[J].AIAA jour-nal,2000,38(2):275-283.
  • 5Erina Murakami,Dimitri Papamoschou.Eddy convection in coaxial supersonic jets[J].AIAA journal,2000,38(4):628-635.
  • 6Srinivasan K,Rathakrishnan E.Studies on polygonal slot jets[J].AIAA,journal 2003,41(10):1985-1987.
  • 7蔡良才.机场规划设计[M].北京:解放军出版社,2002..
  • 8李玉柱,贺五洲.工程流体力学[M].北京:清华大学出版社,2006:71.
  • 9徐学邈,王如根,张相毅,周敏,周向东.射流角度对流体控制矢量喷管的影响[J].空军工程大学学报(自然科学版),2008,9(1):5-8. 被引量:5

引证文献2

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部