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Titlebook: Buckling and Postbuckling of Composite Plates; G. J. Turvey,I. H. Marshall Book 1995 Chapman & Hall 1995 buckling.deformation.finite eleme

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41#
發(fā)表于 2025-3-28 16:01:41 | 只看該作者
42#
發(fā)表于 2025-3-28 20:20:03 | 只看該作者
Landschaften der Bundesrepublikr point supports); variable thickness; and with temperature-dependent material properties. The finite element method has enabled non-linear postbuckling analysis and sensitivity analysis, which can be used to study the sensitivity of the buckling and postbuckling responses to variations in the diffe
43#
發(fā)表于 2025-3-29 00:50:48 | 只看該作者
https://doi.org/10.1007/978-1-349-86035-7ia, certain new material imperfections can be found in composite structures in addition to the better-known imperfections that one finds in metallic structures. Thus, broken fibres, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute ma
44#
發(fā)表于 2025-3-29 04:58:18 | 只看該作者
https://doi.org/10.1007/978-1-349-86035-7tors include the use of discrete ply angles and layer thicknesses, restrained edges, shear deformation, cut-outs, thermal loading, strength and stiffness constraints, multiple design objectives and shape design.
45#
發(fā)表于 2025-3-29 09:23:05 | 只看該作者
Finite element buckling and postbuckling analysesr point supports); variable thickness; and with temperature-dependent material properties. The finite element method has enabled non-linear postbuckling analysis and sensitivity analysis, which can be used to study the sensitivity of the buckling and postbuckling responses to variations in the diffe
46#
發(fā)表于 2025-3-29 14:09:50 | 只看該作者
Delamination buckling of flat laminatesia, certain new material imperfections can be found in composite structures in addition to the better-known imperfections that one finds in metallic structures. Thus, broken fibres, delaminated regions, cracks in the matrix material, as well as holes, foreign inclusions and small voids constitute ma
47#
發(fā)表于 2025-3-29 17:11:34 | 只看該作者
Lay-up optimization of laminated plates under buckling loadstors include the use of discrete ply angles and layer thicknesses, restrained edges, shear deformation, cut-outs, thermal loading, strength and stiffness constraints, multiple design objectives and shape design.
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