Nonlinear dynamic finite element analysis of thick transversly flexible sandwich panel on elastic foundation with account of damage progression in time. Part 1. Three-dimensional formulation and two-dimensional plate theory
In order to construct a plate theory for a thick transversely compressible sandwich plate with composite laminated face sheets, the author makes simplifying assumptions regarding distribution o f transverse strain components in the thickness direction. It is assumed that the transverse strains...
Збережено в:
Видавець: | Інститут проблем міцності ім. Г.С. Писаренко НАН України |
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Дата: | 2005 |
Автор: | |
Формат: | Стаття |
Мова: | English |
Опубліковано: |
Інститут проблем міцності ім. Г.С. Писаренко НАН України
2005
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Назва видання: | Проблемы прочности |
Теми: | |
Онлайн доступ: | http://dspace.nbuv.gov.ua/handle/123456789/47676 |
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Цитувати: | Nonlinear dynamic finite element analysis of thick transversly flexible sandwich panel on elastic foundation with account of damage progression in time. Part 1. Three-dimensional formulation and two-dimensional plate theory / V.Y. Perel // Проблемы прочности. — 2005. — № 2. — С. 92-106. — Бібліогр.: 13 назв. — англ. |
Репозиторії
Digital Library of Periodicals of National Academy of Sciences of UkraineРезюме: | In order to construct a plate theory for a thick
transversely compressible sandwich plate with
composite laminated face sheets, the author
makes simplifying assumptions regarding distribution
o f transverse strain components in the
thickness direction. It is assumed that the transverse
strains, i.e., £xz, £yz, and £zz do not vary
in the thickness direction within the face sheets
and the core, but can be different functions of
the in-plane coordinates in different
sublaminates (the face sheets and the core). An
algorithm, which takes account of damage progression
in dynamic problems, is incorporated
into the computational scheme based on the
geometrically nonlinear formulation, and is applied
to failure analysis o f a sandwich plate under
ground impact. The proposed model o f the
sandwich plate does not require many degrees
o f freedom in the finite element computations
and has a wide range of applicability: it can be
applied to the sandwich plates with a wide
range o f ratios of thickness to the in-plane dimensionswith both thin and thick face sheets
(as compared to the thickness o f the core) and
to the sandwich plates with both transversely
rigid and transversely compressible face sheets
and cores. |
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