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    Fracture behavior of multi-layered composites under impact loading

    , Article Materials Science and Engineering A ; Volume 448, Issue 1-2 , 2007 , Pages 20-24 ; 09215093 (ISSN) Tekyeh Marouf, B ; Bagheri, R ; Sharif University of Technology
    2007
    Abstract
    In this investigation, aluminum layers are bonded together using epoxy adhesive. The adhesive is modified using different additives and the influence of adhesive composition on interfacial fracture energy is measured via double cantilever beam (DCB) test. To characterize the mechanical behavior of the adhesive, compression and impact tests were incorporated. The results of compression and impact tests show that compressive and impact properties of adhesives are functions of type and content of modifier. In the DCB test, it was observed that while addition of rubber particles increase interfacial fracture energy of epoxy, incorporating SiC particles decrease this parameter. Also, the results... 

    Free vibration analysis of multilayered functionally graded composite cylinder

    , Article ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE), 12 November 2010 through 18 November 2010 ; Volume 13 , 2010 , Pages 441-450 ; 9780791844502 (ISBN) Kargarnovin, M. H ; Hashemi, M ; Sharif University of Technology
    Abstract
    Free vibration of multilayered composite cylinder which volume fraction of fiber varies according to power law in longitudinal direction has been studied. Rule of mixture model and reverse of that are employed to represent elastic properties of this fibrous functionally graded composite. Straindisplacement relations employed are based on Reissner- Naghdi-Berry's shell theory. The displacement finite element model of the governing equations of motion is derived by writing weak form of them. The Lagrangian shape functions for in-plane displacements and Hermitian shape functions for displacement in normal direction to the surface of mid-plane are utilized by defining a conformal quadrilateral... 

    Interlaminar stress analysis of composite shell structures using a geometrically nonlinear layer-wise shell finite element

    , Article Composite Structures ; Volume 257 , 2021 ; 02638223 (ISSN) Soltani, Z ; Hosseini Kordkheili, S. A ; Sharif University of Technology
    Elsevier Ltd  2021
    Abstract
    This work aims to calculate interlaminar stress distribution through the thickness of multilayered composite shell structures by employing a novel nonlinear layer-wise shell finite element formulation. Adapting the Mindlin– Reissner theory in each layer, the shear-deformable layer-wise shell element presents the interlaminar shear stress distributions by increasing the number of layers. The interlaminar normal stress distribution is then determined using the finite difference solution of the general form of equilibrium equation in the non-orthogonal curvilinear grid along the Gaussian points. Two boundary conditions at the bottom and the top surfaces are satisfied by adopting the linear...