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Strong formulation finite element method for arbitrarily shaped laminated plates - Part I. Theoretical analysis
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  • Strong formulation finite element method for arbitrarily shaped laminated plates - Part I. Theoretical analysis
  • Strong formulation finite element method for arbitrarily shaped laminated plates - Part I. Theoretical analysis
저자명
Fantuzzi. Nicholas,Tornabene. Francesco
간행물명
Advances in aircraft and spacecraft science
권/호정보
2014년|1권 2호|pp.125-143 (19 pages)
발행정보
테크노프레스
파일정보
정기간행물|ENG|
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

This paper provides a new technique for solving the static analysis of arbitrarily shaped composite plates by using Strong Formulation Finite Element Method (SFEM). Several papers in literature by the authors have presented the proposed technique as an extension of the classic Generalized Differential Quadrature (GDQ) procedure. The present methodology joins the high accuracy of the strong formulation with the versatility of the well-known Finite Element Method (FEM). The continuity conditions among the elements is carried out by the compatibility or continuity conditions. The mapping technique is used to transform both the governing differential equations and the compatibility conditions between two adjacent sub-domains into the regular master element in the computational space. The numerical implementation of the global algebraic system obtained by the technique at issue is easy and straightforward. The main novelty of this paper is the application of the stress and strain recovery once the displacement parameters are evaluated. Computer investigations concerning a large number of composite plates have been carried out. SFEM results are compared with those presented in literature and a perfect agreement is observed.