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

来源：

INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 1996年 / 13卷 / 01期

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.

引用

页码：13 / 23

页数：11

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