Abstract
A three-dimensional model for the mechanics of elastic/hyperelastic materials reinforced with bidirectional fibers is presented in finite elastostatics. This includes the constitutive formulation of matrix–fiber composite system and the derivation of the corresponding Euler equilibrium equation. The responses of the matrix material and reinforcing fibers are characterized, respectively, via the Neo-Hookean model and quadratic strain energy potential of the Green–Lagrange type. These are further refined by the Mooney–Rivlin strain energy model and the high-order polynomial energy potential of fibers to incorporate the nonlinear behaviors of the matrix material and fibers. Within the framework of differential geometry and strain-gradient elasticity, the general kinematics of bidirectional fibers, including the three-dimensional bending of a fiber and twist between the two adjoining fibers, are formulated, and subsequently integrated into the model of continuum deformation. The admissible boundary conditions are also derived by virtue of variational principles and virtual work statement. In particular, a dimension reduction process is applied to the resulting three-dimensional model through which a compatible two-dimensional model describing both the in-plane and out-of-plane deformations of thin elastic films reinforced with fiber mesh is obtained. To this end, model implementation and comparison with the experimental results are performed, indicating that the proposed model successfully predicts key design considerations of fiber mesh reinforced composite films including stress–strain responses, deformation profiles, shear strain distributions and local structure (a unit fiber mesh) deformations. The proposed model is unique in that it is formulated within the framework of differential geometry of surface to accommodate the three-dimensional kinematics of the composite, yet the resulting equations are reframed in the orthonormal basis for enhanced practical unitality and mathematical tractability. Hence, the resulting model may also serve as an alternative Cosserat theory of plates and shells arising in two-dimensional nonlinear elasticity.
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Acknowledgements
This work was supported by the Natural Sciences and Engineering Research Council of Canada via Grant #RGPIN-2022-03613 and the Chung-Ang University Research Grants in 2022. Kim would like to thank Dr. David Steigmann for stimulating his interest in this subject and for discussions concerning the underlying theory.
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Appendix: Finite element analysis of the fourth-order coupled PDE
Appendix: Finite element analysis of the fourth-order coupled PDE
The systems of PDEs in Eqs. (92)–(93) are fourth-order differential equations with coupled nonlinear terms. The case of such less regular PDEs deserves delicate mathematical treatment and is of particular practical interest. Hence, it is not trivial to demonstrate the associated numerical analysis procedures. For preprocessing, Eq. (92) may be recast as
For \(i=1\):
and similarly for \(i=2\) and 3, where
where \(Q=\chi _{1,11},\ R=\chi _{2,11},\) \(T=\chi _{3,11},~C=\chi _{1,1},\) \(D=\chi _{2,1},M=\chi _{3,1},~E=\chi _{1,2},~F=\chi _{2,2},\) \(N=\chi _{3,2},\) \(U=\chi _{1,22,}\) \(V=\chi _{2,22}\) and \(S=\chi _{3,22}\). Hence, the order of differential equations is reduced from the three coupled equations of the fourth order to seventeen coupled equations of the2nd order. Especially, the nonlinear terms in the above equations (e.g., \(A\chi _{2,2},B\chi _{2,1}\) etc...) can be systematically treated via the Picard iterative procedure and/or Newton method;
where the estimated values of A, B continue to be updated based on their previous estimations (e.g., \(A_{1}\) and \(B_{1}\) are refreshed by their previous estimations of \(A_{o}\) and \(B_{o}\)) as iteration progresses and similarly for the rest of nonlinear terms.
Also, the weight forms of Eq. (109) can be found as
Thus, we apply integration by part and the Green–Stokes’ theorem, (e.g. \(\mu \int _{\Omega ^{e}}w_{1}\chi _{1,22}d\Omega =-\mu \int _{\Omega ^{e}}w_{1,2}\chi _{1,2}d\Omega +\mu \int _{\partial \Gamma }w_{1}\chi _{1,2}Nd\Gamma \)) and thereby obtain the following weak forms of Eq. (111)
where \(\Omega \), \(\partial \Gamma \) and \(N\ \) are, respectively, the domain of interest, the associated boundary and the rightward unit normal to the boundary \(\partial \Gamma \) in the sense of the Green–Stokes’ theorem. The unknown potentials of \(\chi _{1},\) \(\chi _{2},\chi _{3},\ Q,\ R,C,D,E,F,T,S,U,V,M,N,\ A\) and B can be expressed in the form of Lagrangian polynomial that
Accordingly, the test function w is found to be
where \(w_{i}\) is the weight of the test function and \(\Psi _{i}(x,y)\) are the associated shape functions; \(\Psi _{1}=\frac{ (x-2)(y-1)}{2},\) \(\Psi _{2}=\frac{x(y-1)}{-2},~\Psi _{3}=\frac{xy}{2} \) and \(\Psi _{4}=\frac{y(x-2)}{-2}\). Invoking Eqs. (113), (112) can be recast in terms of Lagrangian polynomial representation as
Now, for the local stiffness matrices and forcing vectors for each elements, we find
where
and
Thus, the unknown potentials (i.e., \(Q,\ R,C,D,E,F,T,S,U,V,M,N,\ A\) and B) can be expressed as
and similarly for the rest of unknowns.
In the simulation, we employed the following convergence criteria
which demonstrates fast convergence within 12 iterations using FEniCS nonlinear solver (see, Table. 1).
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Kim, C.I.L., Islam, S. & Yang, S. A three-dimensional continuum model for the mechanics of an elastic medium reinforced with fibrous materials in finite elastostatics. Continuum Mech. Thermodyn. 36, 119–153 (2024). https://doi.org/10.1007/s00161-023-01266-0
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DOI: https://doi.org/10.1007/s00161-023-01266-0