Abstract
In this paper, a weak form quadrature element formulation of a geometrically nonlinear shell model is proposed and applied for analysis of laminated composite shell structures. Thickness stretch parameters of the shell are incorporated for introducing 3D constitutive relations in the formulation. A drilling rotation constraint on the basis of polar decomposition of a modified deformation gradient is enforced by the Lagrange multiplier method and employed for implementing spatial finite rotations. The present formulation is shown to be feasible to model complex structures and circumvent locking problems naturally. A series of numerical benchmark examples are presented to demonstrate the validity of the formulation.
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Acknowledgements
The present investigation was performed with the support of the National Natural Science Foundation of China (No. 11702098), the Fundamental Research Funds for the Central Universities (2019MS122) and the China Scholarship Council (201906155033).
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Appendix: Expression of element tangent stiffness matrix
Appendix: Expression of element tangent stiffness matrix
The element tangent stiffness matrix \(\mathbf{K }^{(e)}\) consists of three parts corresponding to \(\mathbf {G}_{\mathrm{int}}^{(e)} \), \(\mathbf {G}_{\mathrm{ext}}^{(e)} \) and \(\mathbf {G}_{c}^{(e)} \) in the element residual force vector as
The element internal tangent stiffness matrix can be derived from Eq. (56) as
The expressions of matrices \(\varvec{\Xi }^{(k+l)}\) are
and
with the sub-matrices
and
With the definition of the vector
the matrix \(\varvec{\Gamma }_{ij}^{(k+l)} \) is written as
where
with \(\mathbf {v}_{(i)}^{(k+l)}\) being the \(i\hbox {th}\) term of \(\mathbf {v}^{(k+l)}\).
By defining the following matrices
the element external tangent stiffness matrix has the form
The element tangent stiffness derived from the kinematic constraint term is presented as
with the matrix
The sub-matrices in Eq. (A.17) are
where
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Zhang, R., Zhong, H., Yao, X. et al. A quadrature element formulation of geometrically nonlinear laminated composite shells incorporating thickness stretch and drilling rotation. Acta Mech 231, 1685–1709 (2020). https://doi.org/10.1007/s00707-019-02606-5
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DOI: https://doi.org/10.1007/s00707-019-02606-5