A Finite Element Failure Model for Notched Laminated Composites Loaded in Compression
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This paper describes a progressive damage failure model which is making an attempt to predict damage growth and ultimate compressive strength of notched laminates subjected to uniaxial compression. A non-linear finite element programme is developed to perform the ply-by-ply stress analysis and numerical results are compared with existing experimental data [1,2]; the agreement is acceptable.
2012 ◽
Vol 5
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pp. 231-239
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2019 ◽
Vol 133
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2016 ◽
Vol 40
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pp. 539-546
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1994 ◽
Vol 208
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pp. 9-17
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2012 ◽
Vol 13
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1979 ◽
Vol 28
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pp. 972-978
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pp. 2265-2270
1997 ◽
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