Abstract:The new improved discrete Kirchhoff quadrilateral element based on the third-order zigzag theory developed earlier by the present authors for the static analysis of composite and sandwich plates is extended for dynamics and assessed for its performance for the free vibration response. The element is free from the shear locking. The finite element formulation is validated by comparing the results for simply supported plates with the analytical Navier solution of the zigzag theory. Comparison of the present resu… Show more
“…These functions satisfy the clamped boundary conditions at 1 0 = x , that is where the same Gram-Schmidt approximation scheme is used as in the previous example (Problem 2.) In addition, a high-fidelity FEA is performed [43] and its results are used as reference solutions.…”
“…These functions satisfy the clamped boundary conditions at 1 0 = x , that is where the same Gram-Schmidt approximation scheme is used as in the previous example (Problem 2.) In addition, a high-fidelity FEA is performed [43] and its results are used as reference solutions.…”
“…The six-node plate element developed is a nonconforming element as the element does not satisfy the normal slope continuity requirement. Thus, Kulkarni and Kapuria [34] indicated that the six-node triangular element [33] underestimated the natural frequencies of the sandwich plates. Therefore, three-node triangular element based on the C 1 -type zig-zag model [18] has been developed for comparison in this paper.…”
Section: Numerical Results and Discussionmentioning
From a theoretical and practical viewpoint, the zigzag theory is well adopted in the analysis of laminated composite structures. Nevertheless, for the available zigzag models, artificial constraints in which the first derivatives of transverse displacement are replaced by the assumed variables have to be employed to avoid C 1 interpolation functions in the finite element implementation. Such artificial constraints violate continuity conditions of interlaminar transverse stresses at interfaces. To avoid using artificial constraints, a C 0-type zigzag model is proposed in this paper. C 0 interpolation functions are only required in the finite element formulation as first derivatives of transverse displacement have all been eliminated from the displacement field based on stress compatibility conditions between plies and on the top and bottom surfaces of the plate. Moreover, the number of variables involved in the proposed zigzag model is less than that of the existing zigzag models, yet accurate results are produced comparable to analytical solutions and three-dimensional finite element results. Effects of ply orientations, boundary conditions and length-to-thickness ratio on displacements and stresses of laminated composite plates have been studied.
“…In Table 8, the first ten circular frequencies, computed with different approaches, are compared with the RZT results. Solution cited as 3D FE [58] is obtained by means of three-dimensional finite element analysis and it can be considered as a reference result. For comparison purposes, solutions are also obtained with FSDT (shear correction factors as in [55]).…”
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