1999
DOI: 10.1016/s0263-8223(00)00046-5
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Composite repairs to rib stiffened panels

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Cited by 70 publications
(28 citation statements)
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“…An optimization of the patch thickness is recommended. Ting et al [1] and Turaga and Ripudaman [9] obtained this conclusion. It is noted that the difference of the stress intensity factor between a single and double symmetric patch is stabilized when the thickness e r is greaten then 2 mm.…”
Section: Resultsmentioning
confidence: 74%
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“…An optimization of the patch thickness is recommended. Ting et al [1] and Turaga and Ripudaman [9] obtained this conclusion. It is noted that the difference of the stress intensity factor between a single and double symmetric patch is stabilized when the thickness e r is greaten then 2 mm.…”
Section: Resultsmentioning
confidence: 74%
“…The stress intensity factor is then reduced by the presence of the patch. Several authors showed that the mode I stress intensity factor of repaired crack, exhibits an asymptotic behaviour as the crack length increases [1][2][3][4][5]. The asymptotic value of the SIF was approximated by Rose [6] by the formulas:…”
Section: Introductionmentioning
confidence: 99%
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“…It is then challenging to derive stress intensity factors and predict the fatigue behavior of the repaired structure. Since the first use of a composite patch to repair damaged aircraft and marine structures [1], progresses have been made to improve the accuracy of prediction methods and the effectiveness of bonded composite patch repair technique [2][3][4][5]. Various numerical methods such as boundary element method, collocation method, finite difference method, finite element method and finite element alternating method have been developed for a better prediction of fracture.…”
Section: Introductionmentioning
confidence: 99%
“…Especially, it was pointed out that SIF at the crack tip as fracture parameter is important for the prediction of the extent of improved performance of a bonded composite repair. The analytical investigations were primarily based on the finite element method, namely Ayatolahi and Hashemi [6], Mitchel et al [7], Jones and Callinan [8], Ting et al [9], Bouiadjra et al [10], Umamaheswar and Singh [11].…”
Section: Introductionmentioning
confidence: 99%