Study of disbond effects in a jointed composite structure under variable ambient temperatures

Jointed composite structures (JCSs) are often used in the marine, automotive and civil engineering industries. In JCS, thin carbon-fiber-reinforced composite laminates are bonded with epoxy adhesives. But, disbonds can occur at the bondinterphase due to variable environmental conditions, cyclic loading, aging, fatigue, amongst others, which may lead to a substantial reduction in load-bearing capacity of the structural assembly. Hence, it is essential to identify these hidden disbonds, and the identification becomes more challenging due to frequent change in ambient temperatures. It is found that the ultrasonic guided wave propagation based inspection technique is suitable for inspection of such complex multilayered structures. The aim of this paper is to investigate the disbond effects on the propagating wave modes in the JCS under variable ambient temperatures. Towards this, a series of finite element based numerical simulation of guided Lamb wave propagation in JCS under variable temperature is carried out in ABAQUS using piezoelectric actuator-sensor transducers. Laboratory experiments are then conducted to investigate the disbond effects and a good agreement is found between the simulation and experimental results.

[1]  S. Peters Handbook of Composites , 1998 .

[2]  V. Giurgiutiu Tuned Lamb Wave Excitation and Detection with Piezoelectric Wafer Active Sensors for Structural Health Monitoring , 2005 .

[3]  Sauvik Banerjee,et al.  Guided wave propagation in a honeycomb composite sandwich structure in presence of a high density core. , 2016, Ultrasonics.

[4]  D. Zenkert,et al.  Handbook of Sandwich Construction , 1997 .

[5]  Emmanuel Moulin,et al.  Radome health monitoring with Lamb waves: experimental approach , 2000 .

[6]  P. Qiao,et al.  Impact analysis of fiber reinforced polymer honeycomb composite sandwich beams , 2007 .

[7]  Wieslaw Ostachowicz,et al.  Online detection of barely visible low-speed impact damage in 3D-core sandwich composite structure , 2018 .

[8]  Sauvik Banerjee,et al.  Theoretical modeling of guided wave propagation in a sandwich plate subjected to transient surface excitations , 2012 .

[9]  S. Tsai,et al.  Composite Materials: Design and Applications , 2002 .

[10]  A. Mal,et al.  Response of an Elastic Plate to Localized Transient Sources , 1985 .

[11]  M. Castaings,et al.  Guided waves propagating in sandwich structures made of anisotropic, viscoelastic, composite materials. , 2003, The Journal of the Acoustical Society of America.

[12]  Anders Nilsson,et al.  Wave propagation in and sound transmission through sandwich plates , 1990 .

[13]  Guoliang Huang,et al.  Guided wave propagation in honeycomb sandwich structures using a piezoelectric actuator/sensor system , 2009 .

[14]  Sauvik Banerjee,et al.  Structural Health Monitoring of Advanced Composites Using Guided Waves , 2017 .

[15]  Tribikram Kundu,et al.  Selection of Lamb modes for detecting internal defects in composite laminates , 1997 .

[16]  Victor Giurgiutiu,et al.  Single Mode Tuning Effects on Lamb Wave Time Reversal with Piezoelectric Wafer Active Sensors for Structural Health Monitoring , 2007 .

[17]  Joseph L. Rose,et al.  Rapid Inspection of Composite Skin-Honeycomb Core Structures with Ultrasonic Guided Waves , 2003 .

[18]  Lowe,et al.  The transmission of Lamb waves across adhesively bonded lap joints , 2000, The Journal of the Acoustical Society of America.

[19]  Rakesh K. Kapania,et al.  FREE VIBRATION ANALYSIS OF LAMINATED PLATES USING A LAYER-WISE THEORY , 1993 .

[20]  N. D. Boffa,et al.  Guided waves in a stiffened composite laminate with a delamination , 2016 .