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- W2321697712 abstract "An approximate solution in the form of a polynomial is developed for the in-plane stresses near a circular hole, in an orthotropic composite laminate under biaxial loading. The derived stresses are found to be in good agreement with the exact anisotropic solution, for a series of laminates investigated. However, the degree of accuracy of the approximate stress distribution is strongly influenced by the laminate layup and the biaxiality ratio. The resultant stresses are then employed in a fracture mechanics model to estimate the damage initiation, growth and final fracture of carbon fibre-epoxy plates with an openhole subjected to biaxial compression-tension static loading. Using the independently measured laminate parameters of unnotched strength and in-plane fracture toughness, the model successfully predicts the notched strength of multidirectio nal laminates under various biaxiality ratios." @default.
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- W2321697712 date "1998-04-20" @default.
- W2321697712 modified "2023-09-24" @default.
- W2321697712 title "Strength prediction of CFRP plates with a hole under biaxial compression-tension" @default.
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- W2321697712 doi "https://doi.org/10.2514/6.1998-1701" @default.
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