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• W4310256200 abstract "The forward swept-wing aircraft is one of the most superior aircrafts in terms of both aerodynamics and structural configurations. This design has been consistently frustrated by the divergence problem. The divergence in the wing can be reduced by increasing the wing bending stiffness which in turn increases the weight of the wing. So, to accomplish both, composite materials are being employed in this analysis. The alteration of the fiber angle orientation enables the material to improve mechanical properties. This research has been conducted to analyze the buckling behavior of different materials with the various fiber angle orientation so that the material would be sufficient to alleviate divergence. A laminate of three different materials, carbon fiber, graphite epoxy and Kevlar epoxy for 20 different stacking sequences, each sequence consisting of 24 plies have been analyzed by using Fortran and Abaqus. The analysis results showed that the graphite epoxy has better mechanical property comparing to the other two materials, and it can be used for divergence elimination." @default.
• W4310256200 created "2022-11-30" @default.
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• W4310256200 date "2022-11-29" @default.
• W4310256200 modified "2023-09-30" @default.
• W4310256200 title "Simulation Analysis of Composite Materials for Divergence Elimination" @default.
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• W4310256200 doi "https://doi.org/10.1007/978-981-19-6032-1_2" @default.
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