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- W2808041593 abstract "Abstract The present work deals with the prediction of failure mode in thin FRP laminates under uniform temperature. The failure occurs either in static or in buckling mode for a thin FRP laminate. A 2-D finite element method that works on classical lamination theory is employed to analyze the structure which in the form of a thin rectangular plate. The problem is modeled in commercial software ANSYS version 12. Effect of plate in-plane aspect ratio (a/b), Fiber stacking sequence ((i) symmetric cross ply, (ii) Quasi-isotropic, and (iii) symmetric angle ply with 45 0 angle) on mode of failure is studied for three different composite materials ((i) E-Glass/Epoxy with V f = 0.55, (ii) Kevlar 49/Epoxy with V f = 0.60, and (iii) Carbon/Epoxy bidirectional fabric with V f = 0.62)." @default.
- W2808041593 created "2018-06-21" @default.
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- W2808041593 date "2018-01-01" @default.
- W2808041593 modified "2023-09-27" @default.
- W2808041593 title "Prediction of Failure mode of thin FRP laminate under Thermal Loading" @default.
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- W2808041593 doi "https://doi.org/10.1016/j.matpr.2018.02.264" @default.
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