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- W2317238630 abstract "The present investigation is devoted to the development of a new optimal design of lateral wing upper covers made of advanced composite materials, with special emphasis on closer conformity of the developed finite element analysis and operational requirements for aircraft wing panels. In the first stage, 24 weight optimization problems based on linear buckling analysis were solved for the laminated composite panels with three types of stiffener, two stiffener pitches and four load levels, taking into account manufacturing, reparability and damage tolerance requirements. In the second stage, a composite panel with the best weight/design performance from the previous study was verified by nonlinear buckling analysis and optimization to investigate the effect of shear and fuel pressure on the performance of stiffened panels, and their behaviour under skin post-buckling. Three rib-bay laminated composite panels with T-, I- and HAT-stiffeners were modelled with ANSYS, NASTRAN and ABAQUS finite element codes to..." @default.
- W2317238630 created "2016-06-24" @default.
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- W2317238630 date "2016-01-14" @default.
- W2317238630 modified "2023-09-27" @default.
- W2317238630 title "Weight optimal design of lateral wing upper covers made of composite materials" @default.
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- W2317238630 doi "https://doi.org/10.1080/0305215x.2015.1128422" @default.
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