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- W1969948791 abstract "Buckling behaviour of a specific skeletal/continuum structure under inplane loading is investigated by numerical and experimental analysis. The basic structure comprises a skeletal system sandwiched between two plates and is connected to the plates at discrete nodal joints. The initial buckling of the system is substantially increased by pretensioning the plates. Two Perspex experimental models have been tested to validate the finite element models and to demonstrate the prestressing technique. A parameter study is then carried out on advanced composite units to evaluate the maximum effect of prestressing on different systems by using different materials for the skeletal members and by the introduction of flanges or rigid foam infill." @default.
- W1969948791 created "2016-06-24" @default.
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- W1969948791 date "1996-01-01" @default.
- W1969948791 modified "2023-09-27" @default.
- W1969948791 title "Buckling of advanced composite prestressed units under inplane loading" @default.
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- W1969948791 doi "https://doi.org/10.1016/1359-835x(96)00011-5" @default.
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