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- W3136756985 abstract "Conic shell structures are widely used in aerospace industries. In the literature various models have been proposed to failure analysis of composite materials. Clearly, each model has a favorable range of applications. In this paper tensile, compressive, shear and thermal expansion properties of tape-wounded Carbon/Phenolic composites are firstly measured at various temperatures in range 23–200°C. The captured properties are then taken into account to progressive failure analysis of a conic Carbon/Phenolic structure under internal pressure and thermal loadings. For this end, a particular failure criterion is proposed to predict failure in the composite structures with a reasonable margin of safety. The enhanced model is then implemented into the commercial finite element software of ABAQUS via a developed user material (UMAT) subroutine utilizing a suitable solution algorithm. Advantages of the model are assessed and comparisons with other failure criteria as well as experiment are presented." @default.
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- W3136756985 date "2021-03-12" @default.
- W3136756985 modified "2023-09-27" @default.
- W3136756985 title "A particular criterion for progressive failure analysis of carbon/phenolic tape-wounded conic shells" @default.
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- W3136756985 doi "https://doi.org/10.1177/1056789521995914" @default.
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