Transient response of a laminated sandwich plate with viscoelastic core subjected to air blast: Theory and experiment

D. Balkan*, O. Acar, H. S. Türkmen, Z. Mecitoǧlu

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2 Atıf (Scopus)

Özet

This paper is focused on the theoretical and experimental study of the dynamic behavior of sandwich composite plates with a viscoelastic core subjected to blast load. The sandwich plate has carbon/epoxy face sheets and an aramid honeycomb core. The clamped boundary conditions are considered for all edges of the plate. The sandwich plate is modeled using first order shear deformation theory considering the geometrical non-linearities. The equations of motion are derived by the use of the virtual work principle for the sandwich plate. The viscoelastic behavior is modeled by using the Kelvin-Voigt theory. The equations of motion are reduced into the time domain using Galerkin's method. The non-linear-coupled equation system is solved by Mathematica Software. In the experimental study, the pressurized air in a shock tube is impinged on the sandwich composite plate by rupturing a membrane in front of the shock tube. The strain-time histories obtained from the theoretical analysis are compared with the experimental ones and a good agreement is found.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıStructures Under Shock and Impact XI, SUSI 2010
Sayfalar113-124
Sayfa sayısı12
DOI'lar
Yayın durumuYayınlandı - 2010
Etkinlik11th International Conference on Structures Under Shock and Impact, SUSI 2010 - Tallinn, Estonia
Süre: 28 Tem 201030 Tem 2010

Yayın serisi

AdıWIT Transactions on the Built Environment
Hacim113
ISSN (Basılı)1743-3509

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???event.eventtypes.event.conference???11th International Conference on Structures Under Shock and Impact, SUSI 2010
Ülke/BölgeEstonia
ŞehirTallinn
Periyot28/07/1030/07/10

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