Micromechanical prediction of damage due to transverse ply cracking under fatigue loading in composite laminates
| Autor: | Amin Farrokhabadi, Milad Rohanifar, Davood Salimi-Majd, Bjian Mohammadi |
|---|---|
| Rok vydání: | 2017 |
| Předmět: |
Materials science
Polymers and Plastics business.industry Mechanical Engineering Micromechanics 02 engineering and technology Structural engineering Composite laminates 021001 nanoscience & nanotechnology Strain energy Cracking Transverse plane 020303 mechanical engineering & transports 0203 mechanical engineering Mechanics of Materials Fatigue loading Energy based Materials Chemistry Ceramics and Composites Laminated composites Composite material 0210 nano-technology business |
| Zdroj: | Journal of Reinforced Plastics and Composites. 36:377-395 |
| ISSN: | 1530-7964 0731-6844 |
| DOI: | 10.1177/0731684416676635 |
| Popis: | To predict the matrix microcracking of laminated composites under fatigue loading, a novel energy based model is presented in the framework of micromechanics. For this purpose, strain energy release rate (SERR) of microcracks which had been derived previously for the whole laminate, is developed for a lamina, and then is calculated using a stress transfer-based stiffness reduction method. The advantages of the proposed method include its capability to predict the matrix cracking of general lay-ups based on the local stresses and stiffnesses of each plies separately and not being limited to a special stacking sequence. In order to predict micro-cracking propagation of composites under cyclic loading, the coefficients of the modified Paris law are extracted using the available experimental data of crack density–cycle curves. Then using multi-scale modelling and continuum damage mechanics concept, the proposed algorithm is implemented in ANSYS finite element software, as a new user defined material (Usermat). The static progress of failure on [45/−45]s laminate is simulated and the obtained results are compared with the existing experimental data in a good agreement. Finally, the results of implemented fatigue algorithm for different cross-ply laminates under different stress levels are obtained and compared with the available experimental data. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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