Symmetric buckling of the composite three-layer plate
Автор: Lopatin A.V., Udaltsov R.A.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Математика, механика, информатика
Статья в выпуске: 2 (28), 2010 года.
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The definition problem of critical forces, which provokes wrinkling of composite base layers of triplex sandwich plate with orthotropic core is solved. A new model of elastic core is offered. It considers elastic core rigidity on compression and shear, and also nonlinear character of decaying of normal displacement throughout the thickness.
Composite plate, buckling, symmetrical
Короткий адрес: https://sciup.org/148176191
IDR: 148176191
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