Nonlinear dynamic behaviour of tapered sandwich plates subjected to blast loading

S. Susler, Z. Kazanci, H. S. Turkmen

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1 Atıf (Scopus)

Özet

The dynamic behaviour of simply supported tapered laminated sandwich plates subjected to the air blast loading is investigated numerically. The theory is based on the classical sandwich plate theory including von Kármán large deformation effects, in-plane stiffness and inertias, and shear deformation. The equations of motion for the plate are derived by the use of the virtual work principle. Approximate solution functions are assumed for the space domain and substituted into the equations. The Galerkin method is used to obtain the nonlinear differential equations in the time domain. The finite difference method is applied to solve the system of coupled nonlinear equations. The displacement-time and strain-time histories are obtained. The theoretical results are compared with ANSYS finite element results and are found to be in an agreement.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıECCM 2012 - Composites at Venice, Proceedings of the 15th European Conference on Composite Materials
YayınlayanEuropean Conference on Composite Materials, ECCM
ISBN (Basılı)9788888785332
Yayın durumuYayınlandı - 2012
Etkinlik15th European Conference on Composite Materials: Composites at Venice, ECCM 2012 - Venice, Italy
Süre: 24 Haz 201228 Haz 2012

Yayın serisi

AdıECCM 2012 - Composites at Venice, Proceedings of the 15th European Conference on Composite Materials

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???event.eventtypes.event.conference???15th European Conference on Composite Materials: Composites at Venice, ECCM 2012
Ülke/BölgeItaly
ŞehirVenice
Periyot24/06/1228/06/12

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