A new 4-node quadrilateral element based on layerwise approach for free vibration analysis of laminate-faced sandwich plates
Abstract
The new quadrilateral element based on the layerwise approach, developed earlier by the present authors for the static analysis of laminated composite and sandwich plates, is extended to study the free vibration behavior of multilayer sandwich plates. The model is based on the third order shear deformation theory for the core and the first order shear deformation theory for the face sheets. Compatibility conditions are imposed at face sheets/core interfaces to satisfy the interlaminar displacement continuity. Unlike the majority of the layerwise models, the number of DOFs is independent of the number of layers. In order to study the free vibration, a consistent mass matrix is adopted in the present formulation. The obtained numerical results by the present model are in excellent agreement with those obtained via analytical solution and numerical results found in the literatureReferences
Belarbi, M. O. (2015) Éléments finis pour l’analyse des structures sandwichs. Thèse de Doctorat, Département de Génie Civil, Université de Biskra.
Belarbi, M. O., & A. Tati (2015) A new C0 finite element model for the analysis of sandwich plates using combined theories. International Journal of Structural Engineering, 6(3): 212-239.
Belarbi M. O, A. Tati, H. Ounis & A. Benchabane (2016) Development of a 2D isoparametric finite element model based on the layerwise approach for the bending analysis of sandwich plates. Structural Engineering and Mechanics 57(3): 473-506.
Chakrabarti, A. & A.H. Sheikh (2004) Vibration of laminate-faced sandwich plate by a new refined element, Journal of Aerospace Engineering, 17 (3): 123-134.
Kant, T. & K. Swaminathan (2001) Analytical solutions for free vibration of laminated composite and sandwich plates based on a higher-order refined theory. Composite Structures 53(1): 73-85.
Kulkarni, S.D. & S. Kapuria (2008) Free vibration analysis of composite and sandwich plates using an improved discrete Kirchhoff quadrilateral element based on third-order zigzag theory. Computational Mechanics, 42 (6): 803-824.
Khechai, A., A. Tati & A, Guettala (2014) Finite element analysis of stress concentrations and failure criteria in composite plates with circular holes. Frontiers of Mechanical Engineering, 9(3): 281-294.
Linke, M., W. Wohlers & H.-G. Reimerdes (2007) Finite element for the static and stability analysis of sandwich plates. Journal of sandwich structures and materials 9(2): 123-142.
Maturi, D. A., A. J. M. Ferreira, A. M. Zenkour & D. S. Mashat (2014). Analysis of sandwich plates with a new layerwise formulation. Composites Part B: Engineering 56(0): 484-489.
Nabarrete, A., S. F. M. De Almeida & J. S. Hansen (2003) Sandwich-plate vibration analysis: three-layer quasi-three-dimensional finite element model. AIAA journal, 41(8): 1547-1555.
Nayak, A., S. J. Moy & R. Shenoi (2003) Quadrilateral finite elements for multilayer sandwich plates. The Journal of Strain Analysis for Engineering Design 38(5): 377-392.
Ounis, H., A. Tati & A. Benchabane (2014) Thermal buckling behavior of laminated composite plates: a finite-element study. Frontiers of Mechanical Engineering, 9(1): 41-49.
Pandey, S. & S. Pradyumna (2015) A new C0 higher-order layerwise finite element formulation for the analysis of laminated and sandwich plates. Composite Structures (131): 1-16.
Ramesh, S. S., C. Wang, J. Reddy & K. Ang (2009) A higher-order plate element for accurate prediction of interlaminar stresses in laminated composite plates. Composite Structures 91(3): 337-357.
Ramtekkar, G., Y. Desai & A. Shah (2003) Application of a three-dimensional mixed finite element model to the flexure of sandwich plate. Computers & Structures 81(22): 2183-2198.
Rao, M., K. Scherbatiuk, Y. Desai & A. Shah (2004) Natural Vibrations of Laminated and Sandwich Plates. Journal of Engineering Mechanics 130(11): 1268-1278.
Sahoo, R. & B. Singh (2014) A new trigonometric zigzag theory for buckling and free vibration analysis of laminated composite and sandwich plates. Composite Structures 117: 316-332.
Zhen, W., C. Wanji & R. Xiaohui (2010) An accurate higher-order theory and C0 finite element for free vibration analysis of laminated composite and sandwich plates. Composite Structures 92(6): 1299-1307.
Belarbi, M. O., & A. Tati (2015) A new C0 finite element model for the analysis of sandwich plates using combined theories. International Journal of Structural Engineering, 6(3): 212-239.
Belarbi M. O, A. Tati, H. Ounis & A. Benchabane (2016) Development of a 2D isoparametric finite element model based on the layerwise approach for the bending analysis of sandwich plates. Structural Engineering and Mechanics 57(3): 473-506.
Chakrabarti, A. & A.H. Sheikh (2004) Vibration of laminate-faced sandwich plate by a new refined element, Journal of Aerospace Engineering, 17 (3): 123-134.
Kant, T. & K. Swaminathan (2001) Analytical solutions for free vibration of laminated composite and sandwich plates based on a higher-order refined theory. Composite Structures 53(1): 73-85.
Kulkarni, S.D. & S. Kapuria (2008) Free vibration analysis of composite and sandwich plates using an improved discrete Kirchhoff quadrilateral element based on third-order zigzag theory. Computational Mechanics, 42 (6): 803-824.
Khechai, A., A. Tati & A, Guettala (2014) Finite element analysis of stress concentrations and failure criteria in composite plates with circular holes. Frontiers of Mechanical Engineering, 9(3): 281-294.
Linke, M., W. Wohlers & H.-G. Reimerdes (2007) Finite element for the static and stability analysis of sandwich plates. Journal of sandwich structures and materials 9(2): 123-142.
Maturi, D. A., A. J. M. Ferreira, A. M. Zenkour & D. S. Mashat (2014). Analysis of sandwich plates with a new layerwise formulation. Composites Part B: Engineering 56(0): 484-489.
Nabarrete, A., S. F. M. De Almeida & J. S. Hansen (2003) Sandwich-plate vibration analysis: three-layer quasi-three-dimensional finite element model. AIAA journal, 41(8): 1547-1555.
Nayak, A., S. J. Moy & R. Shenoi (2003) Quadrilateral finite elements for multilayer sandwich plates. The Journal of Strain Analysis for Engineering Design 38(5): 377-392.
Ounis, H., A. Tati & A. Benchabane (2014) Thermal buckling behavior of laminated composite plates: a finite-element study. Frontiers of Mechanical Engineering, 9(1): 41-49.
Pandey, S. & S. Pradyumna (2015) A new C0 higher-order layerwise finite element formulation for the analysis of laminated and sandwich plates. Composite Structures (131): 1-16.
Ramesh, S. S., C. Wang, J. Reddy & K. Ang (2009) A higher-order plate element for accurate prediction of interlaminar stresses in laminated composite plates. Composite Structures 91(3): 337-357.
Ramtekkar, G., Y. Desai & A. Shah (2003) Application of a three-dimensional mixed finite element model to the flexure of sandwich plate. Computers & Structures 81(22): 2183-2198.
Rao, M., K. Scherbatiuk, Y. Desai & A. Shah (2004) Natural Vibrations of Laminated and Sandwich Plates. Journal of Engineering Mechanics 130(11): 1268-1278.
Sahoo, R. & B. Singh (2014) A new trigonometric zigzag theory for buckling and free vibration analysis of laminated composite and sandwich plates. Composite Structures 117: 316-332.
Zhen, W., C. Wanji & R. Xiaohui (2010) An accurate higher-order theory and C0 finite element for free vibration analysis of laminated composite and sandwich plates. Composite Structures 92(6): 1299-1307.
Published
2016-03-24
How to Cite
BELARBI, Mohamed-Ouejdi et al.
A new 4-node quadrilateral element based on layerwise approach for free vibration analysis of laminate-faced sandwich plates.
Journal of Applied Engineering Science & Technology, [S.l.], v. 2, n. 1, p. 1-7, mar. 2016.
ISSN 2571-9815.
Available at: <https://revues.univ-biskra.dz/index.php/jaest/article/view/1506>. Date accessed: 19 nov. 2024.
Issue
Section
Section C: Geotechnical and Civil Engineering
Keywords
Finite element; Multilayered; Sandwich plates; Free vibration; Interlaminar
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