You are here

A Novel Method for Delamination Detection in Composites

Journal Name:

Publication Year:

Abstract (2. Language): 
Delamination detection in the composite structure based on the vibration responses when excited at the lower modes has been suggested here. It has been observed that the nonlinear interaction between the delaminated layers produce higher harmonics of the exciting frequency. These higher harmonics have observed to be useful for the detection and location of the delamination without comparing the vibration data from the healthy state of the composite structure. The paper presents the observation based on the finite element analysis of a composite plate with and without delamination and then on the experiments on the composite plates with and without delamination.
34-42

REFERENCES

References: 

[1] S. H. Diaz Valdes, and C. Soutis, “Delamination detection in composite laminates from variations of their modal
characteristics,” Journal of Sound and Vibration, vol. 228, no. 18, pp. 1-9, 1999.
[2] A. Paolozzi and I. Peroni, “Detection of Debonding Damage in a Composite Plate through Natural Frequency Variations,”
Journal of Reinforced Plastics and Composites, vol. 9, no. 4, pp. 369-389, 1990.
[3] H. Y. Kim and W. B. Hwang, “Effect of debonding on natural frequency response functions of honeycomb sandwich
beams,” Composite Structures, vol. 55, no. 1, pp. 51-62, 2002.
[4] P. Qiao, K. Lu, W. Lestari, and J. Wang, “Curvature mode shape-based damage detection in composite laminated plates,”
Composite Structures, vol. 80, no. 3, pp. 409-428, 2007.
[5] P. Kudela and W. Ostachowicz, “A Multilayer Delaminated Composite Beam and Plate Elements: Reflections of Lamb
Waves at Delamination,” Mechanics of Advanced Materials and Structures, vol. 16, no. 3, pp. 174-187, 2009.
[6] H. Y. Kim and W. B. Hwang, “Effect of debonding on natural frequency response functions of honeycomb sandwich
beams,” Composite Structures, vol. 55, no. 1, pp. 51-62, 2002.
[7] C. N. Della and D. Shu, “Vibration of beams with two overlapping delaminations in pre-buckled states,” Composites Part
B, vol. 38, no. 2, pp. 109-118, 2007.
[8] Z. Su and L. Ye, “Lamb wave-based quantitative identification of delamination in CF/EP composite structures using
artificial neural algorithm,” Composite Structures, vol. 66, no. 4, pp. 627-637, 2004.
[10] Z. Su, L. Ye, and Y. Lu, “Guided Lamb waves for identification of damage in composite structures: a review,” Journal of
Sound and Vibration, vol. 295, no. 3–5, pp. 753–780, 2006.
[11] H. Luo and S. Hanagud, “Dynamics of Delaminated Beams,” International Journal of Solids and Structures, vol. 37, no. 10,
pp. 1501-1519, 2000.
[12] N. Akhter, H.C. Jung, H. Chang, and K. Kim, “Location of delamination in laminated composite plates by pulsed laser
holography,” Optics and Lasers in Engineering, vol. 47, no. 5, pp. 584-588, 2009.
[13] T. Akira, T. Yuuki, and S. Yoshinobu, “Delamination monitoring of graphite/epoxy laminated composite plate of electric
resistance change method,” Composites Science and Technology, vol. 62, no. 9, pp. 1151-1160, 2002.
[14] A. N. Amr and W. W. El-Dakhakhni, “Non-destructive evaluation of laminated composite plates using dielectrometry
sensors,” Smart Materials and Structures, vol. 18, no. 5, 055014(8pp), 2009.
[15] H. Sohn, G. Park, J. R. Wait, N. P. Limback, and C. R. Farrar, “Wavelet-based active sensing for delamination detection in
composite structures,” Smart Materials Structures, vol. 13, no. 1, pp. 153–160, 2004.
[16] H. W. Park, H. Sohn, K. H. Law, and C. R. Farrar, “Time reversal active sensing for health monitoring of a composite
plate,” Journal of Sound and Vibration, vol. 302, no. 1-2, pp. 50-66, 2007.
[17] A. Ghoshal, A. Chattopadhyay, M. J. Schulz, R. Thornburgh, and K. Waldron, “Experimental investigation of damage
detection in composite material structures using a laser vibrometer and piezoelectric actuators,” Journal of Intelligent
Material Systems and Structures, , vol. 14, no. 8, pp. 521-537, 2003.
[18] S. Wildy, B. Cazzolato, and A. Kotousov, “Detection of Delamination Damage in a Composite Laminate Beam Utilizing the
Principle of Strain Compatibility,” Key Engineering Materials, vol. 417-418, pp. 269-272, 2010.
[19] N. Akhter, H. C. Jung, H. Chang, and K. Kim, “Location of delamination in laminated composite plates by pulsed laser
holography,” Optics and Lasers in Engineering, vol. 47, no. 5, pp. 584-588, 2009.
[20] A. N. Amr and W. W. El-Dakhakhni, “Non-destructive evaluation of laminated composite plates using dielectrometry
sensors,” Smart Materials and Structures, vol. 18, no. 5, 055014(8pp), 2009.
[21] Lin HY, Huang JH, and Ma CC., “Vibration analysis of angle-ply laminated composite plates with an embedded
piezoceramic layer,” IEEE Trans Ultrason Ferroelectr Freq Control., vol. 50, no. 9, pp. 1084-99, Sep 2003.
[22] U. Polimeo, M. Meo, and D. P. Almond, “Smart Nonlinear Acoustic Based Structural Health Monitoring System,”
Advances in Science and Technology, vol. 56, pp. 426-434, 2008.
[23] M. Meo, U. Polimeo, and G. Zumpano, “Detecting Damage in Composite Material using Nonlinear Elastic Wave
Spectroscopy Methods,” Applied Composite Materials, vol. 15, pp. 115-126, 2008.
[24] J. K. Sinha and M. I. Friswell, “Simulation of the Dynamic Response of a Cracked Beam,” Computers and Structures,
vol. 80, no. 18, pp. 1473-1476, 2002.

Thank you for copying data from http://www.arastirmax.com