Effect of stacking sequence of the bonded composite patch on repair performance |
Beloufa, Hadja Imane
(Laboratoire de Modelisation Numerique et Experimentale des Phenomenes Mecaniques, Faculty of Sciences and Technology, University Abdelhamid Ibn Badis of Mostaganem)
Ouinas, Djamel (Laboratoire de Modelisation Numerique et Experimentale des Phenomenes Mecaniques, Faculty of Sciences and Technology, University Abdelhamid Ibn Badis of Mostaganem) Tarfaoui, Mostapha (Laboratoire Brestois de Mecanique et des Systemes, ENSTA Bretagne) Benderdouche, Noureddine (SEA2M, Faculty of Sciences and Technology, University Abdelhamid Ibn Badis of Mostaganem) |
1 | Baker, A. and Jones, R. (1988), Bonded Repair of Aircraft Structures, Martinus Nijhoff, Dordrecht. |
2 | Atluri, S.N. (1997), Structural integrity and durability, Tech Science Press, Forsyth, Georgia, USA. |
3 | Rose, L.R.F. (1982), "A cracked plate repaired by bonded reinforcement", Int. J. Fract.,18, 135-44. DOI |
4 | Chow, W.T. and Atluri, S.N. (1997), "Composite patch repairs of metal structures: adhesive nonlinearity, thermal cycling, and debonding", AIAA J., 35(9), 1528-1535. DOI |
5 | Lena, M.R., Klug, J.C. and Sun, C.T. (1998), "Composite patches as reinforcements and crack arrestors in aircraft structures", J. Aircraft, 35(2), 318-323. DOI |
6 | Ouinas, D., Serier, B. and Bachir Bouiadjra, B. (2003), "Calcul numerique des parametres de rupture d'une plaque fissuree renforcee par un patch metallique circulaire en mode I et mode mixte", Revue des Composites et des Materiaux Avances, 12(2),. |
7 | Baker, A. (1997), "Growth characterisation of fatigue cracks repaired with adhesively bonded boron/epoxy patches", Proceedings of International Conference on Fracture, ICF-9, 117-128. |
8 | Baker, A. and Chester, R.J. (1993), "Recent advances in composite repair technology for metallic aircraft components", Proceedings of the International Conference on Advanced Composite Materials, 45-9. |
9 | Chung, K.H. and Yang, W.H. (2002), "Fracture mechanics analysis of the bonded repair of skin/ stiffener with an inclined central crack", Compos. Struct., 55, 269-76. DOI |
10 | Bachir Bouiadjra, B., Achour, T., Berrahou, M., Ouinas, D. and Feaugas, X. (2010a), "Numerical estimation of the mass gain between double symmetric and single bonded composite repairs in aircraft structures", Mater. Des., 31, 3073-7. DOI |
11 | Bachir Bouiadjra, B. Fekirini, H., Belhouari, M., Serier, B., Benguediab, B. and Ouinas, D. (2010.b), "SIF for double-and single-sided composite repair in mode I and mixed mode", J. Reinf. Plast. Compos., 30, 416-24. |
12 | Albedah, A., Bachir Bouiadjra, B., Aminallah, L., Es-Saheb, M. and Benyahia, F. (2011), "Numerical analysis of the effect of thermal residual stresses on the performances of bonded composite repairs in aircraft structures", Compos. Part B, 42, 511-6. |
13 | Ouinas, D., Hebbar, A., Bachir Bouiadjra, B., Belhouari, M. and Serier, B. (2009), "Numerical analysis of the stress intensity factors for repaired cracks from a notch with bonded composite semicircular patch", Compos. Part B, 40, 804-810. DOI |
14 | Mhamdia, R., Bachir Bouiadjra, B., Ouddad, W., Feaugas, X. and Touzain, S, (2011), "Stress intensity factor for repaired crack with bonded composite patch under thermo-mechanical loading", J. Reinf. Plast. Compos., 30, 416-24. DOI |
15 | Bachir Bouiadjra, B., Belhouari, M. and Serier, B. (2002), "Computation of the stress intensity factor for repaired cracks in mode I and mixed mode", Compos. Struct., 54, 401-406. |
16 | Ouinas, D., Bachir Bouiadjra, B. and Serier, B. (2007), "The effects of disbond on the stress intensity factor of aluminium panels repaired using composite materials", J. Comp. Struct., 78, 278-284. DOI |
17 | Chung, K.H., Tang, W.H. and Cho, M.R. (2000), "Fracture mechanics analysis of cracked plate repaired by composite patch", Key Eng. Mater., 183-187, 43-48. DOI |
18 | Ratwani, M.M. (1978), "Analysis of cracked, adhesively bonded laminated structures", Paper No. 78483R, AIAA/ASME 19th Structures, Structural Dynamics and Materials Conference, Bethesda, MD 988-994. 1290 Avenue of the Americas, New York, NY 10019. |
19 | Denney, J.J. and Mall, S. (1997), "Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch", Eng. Fract. Mech., 57(5), 507-525. DOI |
20 | Ouinas, D. and Hebbar, A. (2010a), "Full width disbonding effect on repaired cracks in aircraft structural panels with bonded composite patches", J. Therm. Compos. Mater., 23, doi: 10.1177/0892705708103403. DOI |
21 | Mhamdia, R., Serier, B., Bachir Bouiadjra, B. and Belhouari, M. (2012), "Numerical analysis of the patch shape effects on the performances of bonded composite repair in aircraft structures", Compos. Part B, 43, 2012, 391-397. DOI |
22 | Ouinas, D. (2010b), "Effect of disbonding between a composite patch and a cracked aluminum plate on the stress intensity factor", J. Reinf. Plast. Compos., 29, doi: 10.1177/0731684409349555. DOI |
23 | Ouinas, D., Bachir Bouiadjra, B., Himouri, S. and Benderdouche, N. (2012), "Progressive edge cracked aluminium plate repaired with adhesively bonded composite patch under full width disbond", Compos. Part B, 43, 805-811. DOI |
24 | Bachir Bouiadjra, B., Oudad, W., Albedah, A., Benyahia, F. and Belhouari, M. (2012), "Effects of the adhesive disbond on the performances of bonded composite repairs in aircraft structures", Mater. Des., 37, 89-95. DOI |
25 | Gu, L., Ram, A., Kasavajhala, M. and Zhao, S. (2011), "Finite element analysis of cracks in aging aircraft structures with bonded composite-patch repairs", Compos. Part B, 42, 505-510. DOI |
26 | Albedah, A., Bachir Bouiadjra, B., Mhamdia, R., Benyahia, F. and Es-Saheb, M. (2010), "Comparison between double and single sided bonded composite repair with circular shape", Mater. Des., 32, 996-1000. |
27 | Srilakshmi, R. and Ramji, M. (2014), "Experimental investigation of adhesively bonded patch repair of an inclined center cracked panel using DIC", J. Reinf. Plast. Compos., 33(12), 1130-1147. |
28 | Ramji, M., Srilakshmi, R. and Bhanu Prakash, M. (2013), "Towards optimization of patch shape on the performance of bonded composite repair using FEM", Compos. Part B, 45, 710-720. DOI |
29 | Ramji, M. and Srilakshmi, R. (2012), Design of composite patch reinforcement applied to mixed-mode cracked panel using finite element analysis, J. Reinf. Plast. Compos., 31(9), 585-595. DOI |
30 | Kashfuddoja, M. and Ramji, M. (2014), "Design of optimum patch shape and size for bonded repair on damaged carbon fibre reinforced polymer panels", Mater. Des., 74, 174-183. |
31 | Bachir Bouiadjra, B., Ouinas, D., Serier, B. and Benderdouche, N. (2008), "Disbond effects on bonded boron/epoxy composite repair to aluminum plates", Compos. Mater. Sci., 42(2), 220-227. DOI |
32 | Chalkley, P. and Rider, A. (2003), "Toughening boron/epoxy bonded joints using the resin film infusion technique", Part A: Appl. Sci. Manuf., 34(4), 341-348. DOI |
33 | Tay, T.E., Chau, F.S. and Er, C.J. (1996), "Bonded boron-epoxy composite repair and reinforcement of cracked aluminium structures", Compos. Struct., 34(3), 339-347. DOI |
34 | Chukwujekwu, O.A., Singh, N., Enemouh, U.E. and Rao, S.V. (2005), "Design, analysis and performance of adhesively bonded composite patch repair of cracked aluminum aircraft panels", Compos. Struct., 71, 258-70. DOI |
35 | ABAQUS/CAE user's manual (2014), Hibbitt, Karlsson & Sorensen, Inc. |
36 | Feddersen, C.E. (1996), "Plane strain crack toughness testing of high strength metallic materials", W.F. Brown and J.E. Srawley, ASTM STP 410, 77-79. |
37 | Smith, R.N.L. (1988), "The solution of mixed-mode fracture problems using the boundary element method", Eng. Anal., 5, 75-80. DOI |
38 | Ouinas, D., Bachir Bouiadjra, B., Achour, B. and Benderdouche, N. (2009), "Modelling of a cracked aluminum plate repaired with composite octagonal patch in mode I and mixed mode", Mater. Des., 30(3), 590-5. DOI |
39 | Ouinas, D., Bachir Bouiadjra, B., Serier, B. and Said-Bekkouche, M. (2007), "Comparison of the effectiveness of boron/epoxy and graphite/epoxy patches for repaired cracks emanating from a semicircular notch edge", Compos, Struct., 80(4), 514-22. DOI |