Experimental validation of a structural health monitoring methodology. Part III. Damage location on an aircraft wing

被引：96

作者：

Manson, G

Worden, K

Allman, D

机构：

[1] Univ Sheffield, Dynam Res Grp, Dept Mech Engn, Sheffield S1 3JD, S Yorkshire, England

[2] QinetiQ, Aerostruct Dept, Mech Sci Sector, Farnborough GU14 0LX, Hants, England

来源：

JOURNAL OF SOUND AND VIBRATION | 2003年 / 259卷 / 02期

基金：

英国工程与自然科学研究理事会;

关键词：

D O I：

10.1006/jsvi.2002.5169

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

This paper documents the third phase of a programme of experimental work which validates a structural health monitoring methodology based on novelty detection. In this paper, an extension of the detection method for damage location is proposed and demonstrated. The structure of interest is a Gnat aircraft wing. Although it was not possible to damage the aircraft, the method was demonstrated by determining which of a set of inspection panels had been removed. (C) 2002 Elsevier Science Ltd. All rights reserved.

引用

页码：365 / 385

页数：21