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Nonlinear response of a sandwich plate subjected to blast load

  • Ali Baş*
  • , Zafer Kazanci
  • , Zahit Mecitoǧlu
  • *Bu çalışma için yazışmadan sorumlu yazar
  • Istanbul Technical University
  • Turkish Air Force Academy

Araştırma çıktısı: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › Hakemli

1 Atıf (Scopus)

Özet

Present work includes in-plane stiffness and inertia effects on the motion of a sandwich plate under blast load. The geometric nonlinearity effects are taken into account with the von Kármán large deflection theory of thin plates. All edges clamped boundary conditions are considered in the analyses. The equations of motion for the plate are derived by the use of the virtual work principle. Approximate solutions are assumed for the space domain and substituted into the equations of motion. Then 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 results of theoretical analyses are obtained.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıAdvances in Aerospace Technology
YayınlayanAmerican Society of Mechanical Engineers (ASME)
Sayfalar169-177
Sayfa sayısı9
ISBN (Basılı)0791842959, 9780791842959
DOI'lar
Yayın durumuYayınlandı - 2008
EtkinlikASME International Mechanical Engineering Congress and Exposition, IMECE 2007 - Seattle, WA, United States
Süre: 11 Kas 2007 → 15 Kas 2007

Yayın serisi

AdıASME International Mechanical Engineering Congress and Exposition, Proceedings
Hacim1

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???event.eventtypes.event.conference???ASME International Mechanical Engineering Congress and Exposition, IMECE 2007
Ülke/BölgeUnited States
ŞehirSeattle, WA
Periyot11/11/07 → 15/11/07

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