An investigation of interfacial stresses in adhesively-bonded single lap joints subject to transverse pulse loading
Debonding in adhesively-bonded lap joints is a detrimental failure mode contingent upon the level of stresses develped in the adhesive. In this work, an analytical model is developed to estimate the peel and shear stresses in an isotropic elastic adhesive in a single lap joint subjected to transvers...
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| Published in | Journal of sound and vibration Vol. 332; no. 7; pp. 1843 - 1858 |
|---|---|
| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
01.04.2013
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| Subjects | |
| Online Access | Get full text |
| ISSN | 0022-460X 1095-8568 |
| DOI | 10.1016/j.jsv.2012.11.008 |
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| Abstract | Debonding in adhesively-bonded lap joints is a detrimental failure mode contingent upon the level of stresses develped in the adhesive. In this work, an analytical model is developed to estimate the peel and shear stresses in an isotropic elastic adhesive in a single lap joint subjected to transverse pulse loads. The proposed analytical model is an extension of the mathematical models developed by He and Rao (Journal of Sound and Vibration 152 (3), (1992) 405–416, 417–425) to study the coupled transverse and longitudinal vibrations of a bonded lap joint system. The adhesive, in this work, is modelled as an elastic isotropic material implemented in Abaqus 6.9−1. The interfacial stresses obtained by finite element simulations were used to validate the proposed analytical model. The maximum peel and shear stresses in the adhesive as predicted by the analytical model were found to correlate well with the maximum stresses predicted by the corresponding numerical models. The peel stresses in the adhesive were found to be higher than shear stresses, a result which is consistent with intuition for transversally loaded joints. The analytical model is able to predict the maxium stresses in the edges where debonding initiates due to the highly asymetrical stress distribution as observed in the finite element simulations and experiment. This phenomenon is consistent with observations made by Vaidya et al. (International Journal of Adhesion & Adhesives 26 (2006) 184–198). The stress distribution under uniformily distributed transverse pulse loading was observed to be similarly asymetric. |
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| AbstractList | Debonding in adhesively-bonded lap joints is a detrimental failure mode contingent upon the level of stresses develped in the adhesive. In this work, an analytical model is developed to estimate the peel and shear stresses in an isotropic elastic adhesive in a single lap joint subjected to transverse pulse loads. The proposed analytical model is an extension of the mathematical models developed by He and Rao (Journal of Sound and Vibration 152 (3), (1992) 405a416, 417a425) to study the coupled transverse and longitudinal vibrations of a bonded lap joint system. The adhesive, in this work, is modelled as an elastic isotropic material implemented in Abaqus 6.9-1. The interfacial stresses obtained by finite element simulations were used to validate the proposed analytical model. The maximum peel and shear stresses in the adhesive as predicted by the analytical model were found to correlate well with the maximum stresses predicted by the corresponding numerical models. The peel stresses in the adhesive were found to be higher than shear stresses, a result which is consistent with intuition for transversally loaded joints. The analytical model is able to predict the maxium stresses in the edges where debonding initiates due to the highly asymetrical stress distribution as observed in the finite element simulations and experiment. This phenomenon is consistent with observations made by Vaidya et al. (International Journal of Adhesion & Adhesives 26 (2006) 184a198). The stress distribution under uniformily distributed transverse pulse loading was observed to be similarly asymetric. Debonding in adhesively-bonded lap joints is a detrimental failure mode contingent upon the level of stresses develped in the adhesive. In this work, an analytical model is developed to estimate the peel and shear stresses in an isotropic elastic adhesive in a single lap joint subjected to transverse pulse loads. The proposed analytical model is an extension of the mathematical models developed by He and Rao (Journal of Sound and Vibration 152 (3), (1992) 405–416, 417–425) to study the coupled transverse and longitudinal vibrations of a bonded lap joint system. The adhesive, in this work, is modelled as an elastic isotropic material implemented in Abaqus 6.9−1. The interfacial stresses obtained by finite element simulations were used to validate the proposed analytical model. The maximum peel and shear stresses in the adhesive as predicted by the analytical model were found to correlate well with the maximum stresses predicted by the corresponding numerical models. The peel stresses in the adhesive were found to be higher than shear stresses, a result which is consistent with intuition for transversally loaded joints. The analytical model is able to predict the maxium stresses in the edges where debonding initiates due to the highly asymetrical stress distribution as observed in the finite element simulations and experiment. This phenomenon is consistent with observations made by Vaidya et al. (International Journal of Adhesion & Adhesives 26 (2006) 184–198). The stress distribution under uniformily distributed transverse pulse loading was observed to be similarly asymetric. |
| Author | Louca, L.A. Nwankwo, E. Soleiman Fallah, A. |
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| References_xml | – reference: L.J. Hart-Smith, Adhesive-bonded Double-Lap Joints, in: Douglas Aircraft Company, McDonnell Corporation, 3855 Lakewood Blvd Long Beach, California, January, 1973. – volume: 24 start-page: 355 year: 2004 end-page: 366 ident: bib23 article-title: Numerical modelling of lap joints bonded with a rate-dependent adhesive publication-title: International Journal of Adhesion and Adhesives – volume: 152 start-page: 417 year: 1992 end-page: 425 ident: bib20 article-title: Vibration analysis of adhesively bonded lap joint, part II: Numerical solution publication-title: Journal of Sound and Vibration – reference: L.J. Hart-Smith, Analysis and Design of Advanced Composite Bonded Joints, in: Douglas Aircraft Company, McDonnell Douglas Corporation, Long Beach, California 90846, 1973. – reference: L.J. Hart-Smith, A. New Aproach to Composite Laminate Strength Prediction, in: Douglas Aircraft Company,McDonell Douglas Corporation, 1989. – volume: 30 start-page: 856 year: 2008 end-page: 869 ident: bib25 article-title: Analytical–numerical study of interfacial stresses in plated beams subjected to pulse loading publication-title: Engineering Structures – volume: 21 start-page: 211 year: 2001 end-page: 220 ident: bib24 article-title: Finite element and experimental studies on single-lap balanced joints in tension publication-title: International Journal of Adhesion and Adhesives – volume: 18 start-page: 350 year: 1980 end-page: 352 ident: bib5 article-title: A comment on two current adhesive lap joint theories publication-title: AIAA Journal – reference: L.J. Hart-Smith, Non-classical Adhesive-bonded Joints in Practical Aerospace Construction, in: Douglas Aircraft Company, McDonnell Douglas Corporation, 3855 Lakewood Blvd, Long Beach, California 90846, 1973. – volume: 44 start-page: 2349 year: 2007 end-page: 2370 ident: bib17 article-title: Fully-coupled nonlinear analysis of single lap adhesive joints publication-title: International Journal of Solids and Structures – volume: 66 start-page: A17 year: 1944 end-page: A27 ident: bib3 article-title: The stresses in cemented joints publication-title: Journal of Applied Mechanics,Transactions of ASME – reference: L.J. Hart-Smith, Design of Adhesively Bonded Joints, in: Douglas Aircraft Company, McDonnell Douglas Corporation, Long Beach, California, USA. – reference: L.J. Hart-Smith, The Role of Biaxical Stresses in Discriminating Between Meaningful and Illusory Composite Failure Theories, in: Douglas Aircraft Company, McDonnell Douglas Corporation, Long Beach California, 1999. – reference: R.A. 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article-title: Experimental–numerical studies of transverse impact response of adhesively bonded lap joints in composite structures publication-title: International Journal of Adhesion and Adhesives doi: 10.1016/j.ijadhadh.2005.03.013 – ident: 10.1016/j.jsv.2012.11.008_bib26 – year: 2002 ident: 10.1016/j.jsv.2012.11.008_bib14 – volume: 66 start-page: A17 year: 1944 ident: 10.1016/j.jsv.2012.11.008_bib3 article-title: The stresses in cemented joints publication-title: Journal of Applied Mechanics,Transactions of ASME doi: 10.1115/1.4009336 – volume: 24 start-page: 355 year: 2004 ident: 10.1016/j.jsv.2012.11.008_bib23 article-title: Numerical modelling of lap joints bonded with a rate-dependent adhesive publication-title: International Journal of Adhesion and Adhesives doi: 10.1016/j.ijadhadh.2003.11.006 – volume: 152 start-page: 405 year: 1992 ident: 10.1016/j.jsv.2012.11.008_bib19 article-title: Vibration analysis of adhesively bonded lap joint, part I: Theory publication-title: 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| Title | An investigation of interfacial stresses in adhesively-bonded single lap joints subject to transverse pulse loading |
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