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Discrete element simulation of transverse cracking during the pyrolysis of carbon fibre reinforced plastics to carbon/carbon composites

机译:碳纤维增强塑料热解为碳/碳复合材料过程中横向裂纹的离散元模拟

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The fracture behavior of fiber-ceramics like carbon/carbon-silicon carbide strongly depends on the initial damage arising during the production process. We study the transverse cracking of the 90° ply in [0/90]_s crossply laminates due to the thermochemical degradation of the matrix material during the carbonization process by means of a discrete element method. The crack morphology strongly depends on the fiber-matrix interface properties, the transverse ply thickness as well as on the carbonization process itself. To model the 90°ply a two-dimensional triangular lattice of springs is constructed where nodes of the lattice represent fibers. Springs with random breaking thresholds model the disordered matrix material and interfaces. The spring-lattice is coupled by interface springs to two rigid bars which capture the two 0° plies or adjacent sublaminates in the model. Molecular dynamics simulation is used to follow the time evolution of the model system. It was found that under gradual heating of the specimen, after some distributed cracking, segmentation cracks occur in the 90°ply which then develop into a saturated state where the ply cannot support additional load. The dependence of the microstructure of damage on the ply thickness and on the disorder in spring properties is also studied. Crack density and porosity of the system are monitored as a function of the temperature and compared to an analytic approach and experiments.
机译:诸如碳/碳-碳化硅之类的纤维陶瓷的断裂行为在很大程度上取决于生产过程中产生的初始损伤。我们通过离散元素方法研究了碳化过程中基质材料的热化学降解,从而研究了[0/90] _s交叉层压板中90°层压板的横向开裂。裂纹的形态在很大程度上取决于纤维-基体的界面特性,横向层厚度以及碳化过程本身。为了模拟90°铺层,构造了一个二维的弹簧三角形三角网格,其中网格的节点代表纤维。具有随机断裂阈值的弹簧为无序的基质材料和界面建模。弹簧格通过界面弹簧耦合到两个刚性杆,这些刚性杆捕获模型中的两个0°层或相邻的子层板。分子动力学模拟用于跟踪模型系统的时间演变。结果发现,在样品逐渐加热下,经过一定程度的开裂后,在90°层中出现了分段裂纹,然后逐渐形成饱和状态,在此状态下层无法承受额外的载荷。还研究了损伤的微观结构对层厚度和弹簧性能无序性的依赖性。系统的裂缝密度和孔隙率随温度而变化,并与分析方法和实验进行比较。

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