Artigo
Structural damage detection in an aeronautical panel using analysis of variance
Registro en:
Mechanical Systems And Signal Processing, v. 52-53, p. 206-216, 2015.
0888-3270
10.1016/j.ymssp.2014.04.015
WOS:000345472500014
1457178419328525
8338952092032444
Autor
Gonsalez, Camila Gianini [UNESP]
Silva, Samuel da [UNESP]
Brennan, Michael J. [UNESP]
Lopes Junior, Vicente [UNESP]
Resumen
This paper describes a procedure for structural health assessment based on one-way analysis of variance (ANOVA) together with Tukey's multiple comparison test, to determine whether the results are statistically significant. The feature indices are obtained from electromechanical impedance measurements using piezoceramic sensor/actuator patches bonded to the structure. Compared to the classical approach based on a simple change of the observed signals, using for example root mean square responses, the decision procedure in this paper involves a rigorous statistical test. Experimental tests were carried out on an aeronautical panel in the laboratory to validate the approach. In order to include uncontrolled variability in the dynamic responses, the measurements were taken over several days in different environmental conditions using all eight sensor/actuator patches. The damage was simulated by controlling the tightness and looseness of the bolts and was correctly diagnosed. The paper discusses the strengths and weakness of the approach in light of the experimental results. (C) 2014 Elsevier Ltd. All rights reserved. Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP) FINEP Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq) Fundação de Amparo à Pesquisa do Estado de Minas Gerais (FAPEMIG) Univ Estadual Paulista, UNESP, Fac Engn Ilha Solteira, Dept Mech Engn, Ilha Solteira, SP, Brazil Univ Estadual Paulista, UNESP, Fac Engn Ilha Solteira, Dept Mech Engn, Ilha Solteira, SP, Brazil