Detection of delamination in cross-ply composite-laminated beams utilizing irregularity of mode shapes

被引:5
作者
Bazardehi, S. R. Kazemi [1 ]
Kouchakzadeh, M. A. [1 ]
机构
[1] Sharif Univ Technol, Dept Aerosp Engn, Tehran, Iran
关键词
laminated beam; delamination detection; modal analysis; irregularity; DAMAGE DETECTION; VIBRATIONS;
D O I
10.1177/0954410011405953
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, irregularities of the mode shapes are utilized to determine the delamination situation in a composite laminated beam. Modal analysis is used to obtain the mode shapes of the beam; afterwards, the mode shapes are filtered to extract their irregularities. Presence of any delamination and its situation (number, size, and location along the length and thickness of the beam) affect the extracted irregularities. Here, detection of delamination is based on these irregularities of the mode shapes. One of the most important advantages of this method is that unlike many other similar methods, in many cases, the mode shapes of the damaged beam are sufficient and the mode shapes of the intact beam are not required. The method is validated by utilizing the analytical and numerical data for a delaminated beam model. As it will be illustrated, the method can be applied to obtain a very reasonable approximation on the presence of delamination, its size, its location along the length, and number of delaminations for various boundary conditions. In addition, the results show that at least about 15 points of data measurement are required along the length of the beam, and the interval of the points should not exceed 1.5 times the delamination size to be detected.
引用
收藏
页码:1302 / 1309
页数:8
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