A BRIEF SURVEY OF TRANSFER MATRIX TECHNIQUES WITH SPECIAL REFERENCE TO ANALYSIS OF AIRCRAFT PANELS

被引：73

作者：

LIN, YK

DONALDSON, BK

机构：

[1] Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL

[2] Department of Aerospace Engineering, University of Maryland, College Park, MD

来源：

JOURNAL OF SOUND AND VIBRATION | 1969年 / 10卷 / 01期

关键词：

D O I：

10.1016/0022-460X(69)90132-1

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

This article first offers a brief survey of the transfer matrix method of analyzing the dynamic behavior of beam structures. This survey serves as an introduction to the application of the transfer matrix method to single rows of aircraft panels which are continuous over supporting stringers. The skin-stringer problem, important to the prediction of fatigue failures, is discussed for rather general conditions. The panel thickness, length and radii of curvature may vary from panel to panel, and the stringers may have different cross-sectional properties. © 1969.

引用

页码：103 / +

页数：1