Nonlinear response of a sandwich plate subjected to blast load

Ali Bas; Zafer Kazanci; Zahit Mecitoglu

doi:10.1115/IMECE200741152

Nonlinear response of a sandwich plate subjected to blast load

Ali Bas
, Zafer Kazanci
, Zahit Mecitoglu

Uzay Mühendisliği Bölümü

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

5 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 dil	İngilizce
Ana bilgisayar yayını başlığı	Advances in Aerospace Technology
Yayınlayan	American Society of Mechanical Engineers (ASME)
Sayfalar	169-177
Sayfa sayısı	9
ISBN (Elektronik)	0791842959
DOI'lar	https://doi.org/10.1115/IMECE200741152
Yayın durumu	Yayınlandı - 2007
Etkinlik	ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007 - Seattle, United States Süre: 11 Kas 2007 → 15 Kas 2007

Yayın serisi

Adı	ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)
Hacim	1

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007
Ülke/Bölge	United States
Şehir	Seattle
Periyot	11/11/07 → 15/11/07

Bibliyografik not

Publisher Copyright:
Copyright © 2007 ASME & The Boeing Company.

Belgeye Erişim

10.1115/IMECE200741152

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

@inproceedings{151373b28ae04ef799c281b0794471e5,

title = "Nonlinear response of a sandwich plate subjected to blast load",

abstract = "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 K{\'a}rm{\'a}n 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.",

author = "Ali Bas and Zafer Kazanci and Zahit Mecitoglu",

note = "Publisher Copyright: Copyright {\textcopyright} 2007 ASME \& The Boeing Company.; ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007 ; Conference date: 11-11-2007 Through 15-11-2007",

year = "2007",

doi = "10.1115/IMECE200741152",

language = "English",

series = "ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)",

publisher = "American Society of Mechanical Engineers (ASME)",

pages = "169--177",

booktitle = "Advances in Aerospace Technology",

address = "United States",

}

Bas, A, Kazanci, Z & Mecitoglu, Z 2007, Nonlinear response of a sandwich plate subjected to blast load. in Advances in Aerospace Technology. ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE), hac. 1, American Society of Mechanical Engineers (ASME), pp. 169-177, ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007, Seattle, United States, 11/11/07. https://doi.org/10.1115/IMECE200741152

Nonlinear response of a sandwich plate subjected to blast load. / Bas, Ali; Kazanci, Zafer; Mecitoglu, Zahit.
Advances in Aerospace Technology. American Society of Mechanical Engineers (ASME), 2007. p. 169-177 (ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE); Hac. 1).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - Nonlinear response of a sandwich plate subjected to blast load

AU - Bas, Ali

AU - Kazanci, Zafer

AU - Mecitoglu, Zahit

PY - 2007

Y1 - 2007

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/79955524588

U2 - 10.1115/IMECE200741152

DO - 10.1115/IMECE200741152

M3 - Conference contribution

AN - SCOPUS:79955524588

T3 - ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)

SP - 169

EP - 177

BT - Advances in Aerospace Technology

PB - American Society of Mechanical Engineers (ASME)

T2 - ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007

Y2 - 11 November 2007 through 15 November 2007

ER -

Nonlinear response of a sandwich plate subjected to blast load

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Yayın serisi

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