State-based peridynamics method of physical nonlinear simulation of fiber reinforced composite material
A composite material and fiber reinforced technology, which is applied in the realization of physical nonlinear behaviors, can solve problems such as application of examples that have not been seen, and achieve the effect of reducing errors.
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Embodiment 1
[0038]This example is a verification of the compensation-amendment method described in the Summary of the Invention.
[0039] Such as figure 1 As shown, this embodiment includes:
[0040] a) Enter model parameters.
[0041] In this embodiment, the isotropic material plate is subjected to tension and shear displacement fields. The size of the plate of isotropic material is 3.5 mm x 3.5 mm. Elastic modulus of tension and compression E=2.054×10 5 MPa, shear modulus G=7.9×10 4 MPa, Poisson's ratio v=0.3.
[0042] b) Discretization of the model.
[0043] Discretize the model uniformly, take the distance between material points Δx=0.5mm, and the range of near field δ=3Δx.
[0044] c) Try adding a displacement field.
[0045] Apply a pure tensile displacement field, the displacement parameter is: u=ε x x,v=0,ε x = 0.01. figure 2 It is the comparison of the calculation results of the elastic strain energy density function under the tensile displacement field.
[0046] A p...
Embodiment 2
[0048] Such as figure 1 As shown, this embodiment includes the following steps.
[0049] a) Input model parameters
[0050] In this embodiment, the unidirectional composite material plate is subjected to off-axis tensile load. The composite board is 190.5mm long and 19.0mm wide. The included angle between the fiber direction of the laminate and the direction of the load is θ, and the θ angles are 15°, 30°, 45°, and 90°, respectively. Fiber direction modulus E 1 is 127.6GPa, the modulus E perpendicular to the fiber direction 2 10.3GPa, shear modulus G 12 6.0GPa, Poisson's ratio ν 12 is 0.32. The nonlinear constitutive adopts the model proposed by Sun C T and Chen J L in A simple flow rule for characterizing nonlinear behavior of fiber composites[J].Journal of Composite Materials,1989,23:1009-1020. The model parameters are a66=1.5, n=7.0, A=2.794×10 ‐18 (Mpa) ‐n .
[0051] b) Model discretization
[0052] Discretize the model uniformly, take the distance between mate...
Embodiment 3
[0059] Such as figure 1 As shown, this embodiment includes the following steps.
[0060] a) Input model parameters
[0061] In this embodiment, the cross-ply composite board is subjected to off-axis tensile load. The layup of the laminate is [±45] 2S . The laminate is 140.0mm long and 25.0mm wide. Fiber direction modulus E 1 is 66.28GPa, the modulus E perpendicular to the fiber direction 2 66.48GPa, shear modulus G 12 4.54GPa, Poisson's ratio ν 12 is 0.056. The nonlinear constitutive adopts the model proposed by Sun C T and Chen J L in A simple flow rule for characterizing nonlinear behavior of fibercomposites[J].Journal of Composite Materials,1989,23:1009-1020. The model parameters are a66=1.0, n=3.1, A=3.0×10 ‐9 (Mpa) ‐n .
[0062] b) Model discretization
[0063] Discretize the model uniformly, take the distance between material points Δx=0.5mm, and the range of near field δ=3Δx.
[0064] c) Try to add the displacement field, and use the compensation-correctio...
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