A new technique to optimize the use of mode shape derivatives to localize damage in laminated composite plates

Abstract Damage localization in laminated composite structures is a very active area of research due to the role that these kind of structures play in the transport industries. The mode shape derivatives, like rotations (first derivative), curvatures (second derivative) and, more recently, third and four derivatives, have been used to localize damage in composite plates. The most used method to compute these derivatives is the application of finite differences. However, finite differences present several well-known problems, such as the error propagation and amplification. The magnitude of the error associated with the computed derivative is not easy to estimate, mainly because the numerical error associated with finite differences depends on the values of derivatives of higher order than the order of the derivative that one wants to compute. A new technique based on the Ritz method to estimate this error is proposed in this paper. The optimal spatial sampling for the numerical differentiation of the mode shapes are defined based on the minimization of the total error. The good performance of the optimal sampling is shown by applying it to the damage localization in a laminated composite plate.

[1]  Pizhong Qiao,et al.  Curvature mode shape-based damage detection in composite laminated plates , 2007 .

[2]  J. Reddy Mechanics of laminated composite plates and shells : theory and analysis , 1996 .

[3]  Arun Kumar Pandey,et al.  Damage detection from changes in curvature mode shapes , 1991 .

[4]  Timothy M. Whalen,et al.  Experimental validation of the higher‐order derivative discontinuity method for damage identification , 2008 .

[5]  Pizhong Qiao,et al.  Vibration-based Damage Identification Methods: A Review and Comparative Study , 2011 .

[6]  Mohamed Abdel-Basset Abdo,et al.  Damage detection in plate-like structures using High-Order mode shape derivatives , 2012 .

[7]  Nejat Olgac,et al.  Improved numerical computation of uniform beam characteristic values and characteristic functions , 1982 .

[8]  Timothy M. Whalen,et al.  The behavior of higher order mode shape derivatives in damaged, beam-like structures , 2008 .

[9]  Edward Sazonov,et al.  Optimal spatial sampling interval for damage detection by curvature or strain energy mode shapes , 2005 .

[10]  Muneo Hori,et al.  A NUMERICAL STUDY OF STRUCTURAL DAMAGE DETECTION USING CHANGES IN THE ROTATION OF MODE SHAPES , 2002 .

[11]  José Viriato Araújo dos Santos,et al.  EIGENFRE-QUENCY ANALYSIS OF COMPLETELY FREE MULTILAYERED RECTANGULAR PLATES USING A HIGHER-ORDER MODEL AND RITZ TECHNIQUE , 1998 .

[12]  A. Gallego,et al.  Modal analysis of delaminated composite plates using the finite element method and damage detection via combined Ritz/2D-wavelet analysis , 2013 .

[13]  Charles R. Farrar,et al.  A summary review of vibration-based damage identification methods , 1998 .

[14]  C. M. Mota Soares,et al.  A numerical-experimental method for damage location based on rotation fields spatial differentiation , 2011 .

[15]  H. Lopes,et al.  Damage Localisation in Composite Laminated Plates using Higher Order Spatial Derivatives , 2012 .

[16]  H. Abdul Razak,et al.  Determination of damage location in RC beams using mode shape derivatives , 2006 .

[17]  A. M. R. Ribeiro,et al.  A review of vibration-based structural health monitoring with special emphasis on composite materials , 2006 .

[18]  H. Lopes,et al.  A damage localisation method based on higher order spatial derivatives of displacement and rotation fields , 2011 .

[19]  C. M. Mota Soares,et al.  Damage localization in laminated composite plates using mode shapes measured by pulsed TV holography , 2006 .

[20]  Leif A. Carlsson,et al.  Experimental characterization of advanced composite materials , 1987 .

[21]  Milton Abramowitz,et al.  Handbook of Mathematical Functions with Formulas, Graphs, and Mathematical Tables , 1964 .

[22]  Grant P. Steven,et al.  VIBRATION-BASED MODEL-DEPENDENT DAMAGE (DELAMINATION) IDENTIFICATION AND HEALTH MONITORING FOR COMPOSITE STRUCTURES — A REVIEW , 2000 .

[23]  C. M. Mota Soares,et al.  Structural Damage Identification: A Survey , 2008 .

[24]  E. Peter Carden,et al.  Vibration Based Condition Monitoring: A Review , 2004 .

[25]  P. S. Frederiksen,et al.  Single-layer plate theories applied to the flexural vibration of completely free thick laminates , 1995 .