Steel and Composite Structures

  • 제17권3호
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  • Pages.305-320
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  • 2014
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  • 1229-9367(pISSN)
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  • 1598-6233(eISSN)
테크노프레스 (Techno-Press)
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DOI QR코드

DOI QR Code

Buckling of symmetrically laminated quasi-isotropic thin rectangular plates

  • Altunsaray, Erkin (Institute of Marine Science and Technology, Dokuz Eylul University) ;
  • Bayer, Ismail (Department of Naval Architecture and Marine Engineering, Yildiz Technical University)
  • 투고 : 2013.10.31
  • 심사 : 2014.03.23
  • 발행 : 2014.09.25
⟨ 이전 논문 다음 논문 ⟩

초록

The lowest critical value of the compressive force acting in the plane of symmetrically laminated quasi-isotropic thin rectangular plates is investigated. The critical buckling loads of plates with different types of lamination and aspect ratios are parametrically calculated. Finite Differences Method (FDM) and Galerkin Method are used to solve the governing differential equation for Classical Laminated Plate Theory (CLPT). The results calculated are compared with those obtained by the software ANSYS employing Finite Elements Method (FEM). The results of Galerkin Method (GM) are closer to FEM results than those of FDM. In this study, the primary aim is to conduct a parametrical performance analysis of proper plates that is typically conducted at preliminary structural design stage of composite vessels. Non-dimensional values of critical buckling loads are also provided for practical use for designers.

키워드

참고문헌

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