Mechanical characterization and modeling of the deformation and failure of the highly crosslinked RTM6 epoxy resin

被引:66
|
作者
Morelle, X. P. [1 ]
Chevalier, J. [1 ]
Bailly, C. [2 ]
Pardoen, T. [1 ]
Lani, F. [1 ]
机构
[1] Catholic Univ Louvain, Inst Mech Mat & Civil Engn, Pl St Barbe 2,L5-02-02, B-1348 Louvain, Belgium
[2] Catholic Univ Louvain, Inst Condensed Matter & Nanosci, Croix Sud 1,L7-04-02, B-1348 Louvain, Belgium
关键词
RTM6; Highly crosslinked epoxy resin; Elasto-viscoplasticity; Fracture criterion; Constitutive modeling; Aerospace composite; AMORPHOUS GLASSY-POLYMERS; NONLINEAR VISCOELASTIC BEHAVIOR; CONSTITUTIVE MODEL; PLASTIC-DEFORMATION; COUPLED THEORY; STRAIN-RATE; STRESS; FRACTURE; FINITE; SHEAR;
D O I
10.1007/s11043-016-9336-6
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The nonlinear deformation and fracture of RTM6 epoxy resin is characterized as a function of strain rate and temperature under various loading conditions involving uniaxial tension, notched tension, uniaxial compression, torsion, and shear. The parameters of the hardening law depend on the strain-rate and temperature. The pressure-dependency and hardening law, as well as four different phenomenological failure criteria, are identified using a subset of the experimental results. Detailed fractography analysis provides insight into the competition between shear yielding and maximum principal stress driven brittle failure. The constitutive model and a stress-triaxiality dependent effective plastic strain based failure criterion are readily introduced in the standard version of Abaqus, without the need for coding user subroutines, and can thus be directly used as an input in multi-scale modeling of fibre-reinforced composite material. The model is successfully validated against data not used for the identification and through the full simulation of the crack propagation process in the V-notched beam shear test.
引用
收藏
页码:419 / 454
页数:36
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