Abstract
Geometrically nonlinear analysis of shell structures is conducted using weak form quadrature elements. A new geometrically exact shell formulation incorporating drilling degrees of freedom is established wherein rotation quaternions in combination with a total Lagrange updating scheme are employed for rotation description. An extended kinematic condition to serve as the drilling rotation constraint, derived from polar decomposition of modified mid-surface deformation gradient, is exactly satisfied in the formulation. Several benchmark examples are presented to illustrate the versatility and robustness of the present 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 Project funded by China Postdoctoral Science Foundation (No. 2017M612650) and the Fundamental Research Funds for the Central Universities (No. 2017BQ096).
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Appendix: Expression of element tangent stiffness matrix
Appendix: Expression of element tangent stiffness matrix
Corresponding to the vectors \( {\mathbf{G}}_{int}^{(e)} \) and \( {\mathbf{G}}_{c}^{(e)} \) composing the element residual force vector, the element tangent stiffness matrix is written as
It can be derived from Eq. (43) that
where
and
with
The element tangent stiffness matrix related to extended kinematics constraint is obtained from Eq. (56) as
with the matrix
By introducing the matrix
the sub-matrices in Eq. (77) are given by
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Zhang, R., Zhong, H. & Yao, X. A weak form quadrature element formulation of geometrically exact shells incorporating drilling degrees of freedom. Comput Mech 63, 663–679 (2019). https://doi.org/10.1007/s00466-018-1615-4
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DOI: https://doi.org/10.1007/s00466-018-1615-4