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迎风─线性棱边单元法
引用本文:余海涛,邵可然,周克定. 迎风─线性棱边单元法[J]. 中国电机工程学报, 1996, 0(2)
作者姓名:余海涛  邵可然  周克定
作者单位:华中理工大学电机教研室
摘    要:运动导体的涡流问题通常采用迎风─伽辽金法求解,因为采用普通的有限元法求解,解会发生振荡。这种迎风─伽辽金法不适应离散以场矢量H为变量的数学模型。为此本文提出了迎风─线性棱边元法,这种方法具有线性棱元的特点,使用的迎风因子要比迎风─伽辽金法的要少,并且能获得稳定解。文章最后以电磁轨道炮为例,求出电流密度分布,并比较两种方法的结果。

关 键 词:涡流问题,电磁场,迎风─线性棱边单元法,电磁轨道炮

Upwind-Linear Edge Elements Method
Yu Haitao,Shao Keran,Zhou Keding. Upwind-Linear Edge Elements Method[J]. Proceedings of the CSEE, 1996, 0(2)
Authors:Yu Haitao  Shao Keran  Zhou Keding
Affiliation:Huazhong University of Science and TechnologyWhuan 430074 China
Abstract:The Upwind-linear edge element method,which can eliminates the non-physical oscillation in solution, is presented for 3D eddy current problems involving the moving conductors. The numerical method uses fewer upwind factors than the conventional upwind method, and maintains the continuity of the tangential field component and increases the solution accuracy. The proposed method is employed to discretize the 3D eddy current formulation that uses magnetic field intensity H as a variable in whole solution region. As an example the eddy current problems in electromagnetic railgun are used to validate the described method.
Keywords:upwind-linear edge elements  electromagnetic railgun  eddy current  elecromagnetic field  
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