2001
DOI: 10.1299/jsmea.44.282
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Ply-Cracking Damage Theory for Cross-Ply Laminate and Its Application to Finite Element Method.

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Cited by 4 publications
(5 citation statements)
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“…The ply-crack density means a number of ply-through cracks per 1cm length perpendicular to the fiber direction in each ply, and for 30˚ tensile tests it is converted from a number of cracks observed on the specimen edges. Features on the stress-strain relations and ply-cracking damage are almost the same as the results already reported in the references [10,11]. Under on-axis tension, the stress-strain relations are linear up to a knee-point corresponding to the initiation of ply-cracking in 90˚ plies, and then slightly nonlinear with evolution of the ply-cracking damage and delamination.…”
Section: Tensile Properties and Ply-cracking Damage Of Cross-ply Lamisupporting
confidence: 86%
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“…The ply-crack density means a number of ply-through cracks per 1cm length perpendicular to the fiber direction in each ply, and for 30˚ tensile tests it is converted from a number of cracks observed on the specimen edges. Features on the stress-strain relations and ply-cracking damage are almost the same as the results already reported in the references [10,11]. Under on-axis tension, the stress-strain relations are linear up to a knee-point corresponding to the initiation of ply-cracking in 90˚ plies, and then slightly nonlinear with evolution of the ply-cracking damage and delamination.…”
Section: Tensile Properties and Ply-cracking Damage Of Cross-ply Lamisupporting
confidence: 86%
“…Although the stress for ply-cracking initiation in each direction can be roughly predicted by the present method, the predictions are low in the 0.5-3ply, and high in the 2-12 ply and 2-18 ply as compared with the experimental results. This is attributed to that the residual stresses in cross-ply laminates created in the curing process are not considered in the present prediction, and that the present method can not take into consideration an influence of ply thickness, different from prediction based on the energy release rate criterion [10,11]. Fig.…”
Section: Tensile Properties and Ply-cracking Damage Of Cross-ply Lamimentioning
confidence: 92%
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“…Therefore, the damage and nonlinear deformation should be considered in the mechanics and strength evaluation of the laminated composites. From this point of view, many investigations have been carried out on the interlaminar and splitting fracture toughness [1][2][3][4], the damage initiation and evolution under monotonic or cyclic loading [5][6][7][8][9][10][11][12][13], the nonlinear deformation, the damage model and the constitutive relations for the laminated composites [14][15][16][17][18].…”
Section: Introductionmentioning
confidence: 99%
“…In the previous reports [10,11,18], the progressive ply-cracking damage and nonlinear deformation of CFRP cross-ply laminates under axial and off-axis tension were investigated. From the experimental and numerical results, the following conclusions were obtained.…”
Section: Introductionmentioning
confidence: 99%