Numerical analysis of the effect of thermal residual stresses on the performances of bonded composite repairs in aircraft structures
In this study the finite element method is used to analyse the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress-intensity factor at the crack tip is chosen as fracture criterion in order to es...
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| Veröffentlicht in: | Composites. Part B, Engineering Engineering, 2011-04, Vol.42 (3), p.511-516 |
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| container_title | Composites. Part B, Engineering |
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| creator | Albedah, A. Bachir Bouiadjra, B. Aminallah, L. Es-Saheb, M. Benyahia, F. |
| description | In this study the finite element method is used to analyse the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress-intensity factor at the crack tip is chosen as fracture criterion in order to estimate the repair performances. The obtained results show that the presence of the thermal residual stresses reduces considerably the repair performances and consequently decreases the fatigue life of cracked structures. The effects of the curing temperature, the adhesive properties and the adhesive thickness on the stress-intensity factor (SIF) variation with thermal stresses are also analysed. |
| doi_str_mv | 10.1016/j.compositesb.2010.11.013 |
| format | Article |
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The stress-intensity factor at the crack tip is chosen as fracture criterion in order to estimate the repair performances. The obtained results show that the presence of the thermal residual stresses reduces considerably the repair performances and consequently decreases the fatigue life of cracked structures. The effects of the curing temperature, the adhesive properties and the adhesive thickness on the stress-intensity factor (SIF) variation with thermal stresses are also analysed.</description><identifier>ISSN: 1359-8368</identifier><identifier>EISSN: 1879-1069</identifier><identifier>DOI: 10.1016/j.compositesb.2010.11.013</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>adhesion ; Adhesives ; aircraft ; Aircraft industry. Spacecraft ; Aircraft structures ; Application fields ; Applications ; Applied sciences ; B. Adhesion ; B. Residual stress ; B. Stress transfer ; Bonded composite repair ; C. 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Spacecraft</subject><subject>Aircraft structures</subject><subject>Application fields</subject><subject>Applications</subject><subject>Applied sciences</subject><subject>B. Adhesion</subject><subject>B. Residual stress</subject><subject>B. Stress transfer</subject><subject>Bonded composite repair</subject><subject>C. Finite element analysis (FEA)</subject><subject>Curing</subject><subject>Engineering techniques in metallurgy. Applications. Other aspects</subject><subject>equipment performance</subject><subject>Exact sciences and technology</subject><subject>fatigue strength</subject><subject>Fracture mechanics</subject><subject>Maintenance</subject><subject>Mathematical models</subject><subject>Metals. 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| identifier | ISSN: 1359-8368 |
| ispartof | Composites. Part B, Engineering, 2011-04, Vol.42 (3), p.511-516 |
| issn | 1359-8368 1879-1069 |
| language | eng |
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| source | Elsevier ScienceDirect Journals Complete |
| subjects | adhesion Adhesives aircraft Aircraft industry. Spacecraft Aircraft structures Application fields Applications Applied sciences B. Adhesion B. Residual stress B. Stress transfer Bonded composite repair C. Finite element analysis (FEA) Curing Engineering techniques in metallurgy. Applications. Other aspects equipment performance Exact sciences and technology fatigue strength Fracture mechanics Maintenance Mathematical models Metals. Metallurgy Polymer industry, paints, wood Repairing Residual stress Technology of polymers temperature thermal stress |
| title | Numerical analysis of the effect of thermal residual stresses on the performances of bonded composite repairs in aircraft structures |
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