Variable-domain finite element method based on variational principles for solving hybrid problems of fully 3-D compressible rotor flow

被引:0
|
作者
Yan, S [1 ]
Liu, GL [1 ]
机构
[1] SHANGHAI UNIV, SHANGHAI 200072, PEOPLES R CHINA
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Based on a unified variable-domain variational theory (Liu, 1988), a new finite element method (FEM) with self-adjusting nodes for determining the unknown boundaries (shape of the blade and of the annulus walls) in hybrid problems is presented. Two hybrid problem types H(A)xD and [H-C+D]xD are tested numerically by this FEM and the geometry of the rotor bladings thus obtained coincides with the original one quite well. Thus, a new numerical method with great generality and versatility for practical 3-D blading design and/or modification is provided.
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页码:13 / 23
页数:11
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