An effective method for analyzing the effect of structural asymmetry on dynamics of an aircraft

被引：0

作者：

Liu, JK ^{[1
]}

Chan, HC ^{[1
]}

机构：

[1] Zhongshan Univ, Dept Mech, Guangzhou 510275, Peoples R China

来源：

ICVE'98: PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON VIBRATION ENGINEERING, VOL I | 1998年

关键词：

flutter; aircraft; structural asymmetry; direction derivative;

D O I：

暂无

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

An effective method for the analysis of asymmetric effects is presented in this paper. The method is a kind of "direction derivative" technique and can be easily applied to predict whether the structural asymmetry increases or decreases the flutter speed of an aircraft with external stores. As a result, the varying tendency of the flutter speed can be obtained, which is very useful to the designers. The validity and effectiveness of the proposed method are proved analytically.

引用

页码：111 / 113

页数：3

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