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On matrix crack evolution of cross-ply ceramic matrix composite

机译:多层陶瓷基复合材料的基体裂纹演变

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The matrix crack evolution of cross-ply ceramic matrix composites under uniaxial tensile loading has been investigated using the energy balance method. When cross-ply ceramic matrix composites are under tensile loading, transverse cracking in 90° ply and matrix cracking in 0° ply occur. The damage states in cross-ply laminates can be classified into five modes. The cracking mode 3 contains transverse cracking, matrix cracking and fiber/matrix interface debonding. The cracking mode 5 only contains matrix cracking and fiber/matrix interface debonding. The cracking stress of mode 3 and 5 appearing between two existing transverse crack is determined. And the multiple matrix crack evolution of mode 3 has been determined. The effects of ply thickness, fiber volume fraction, interface shear stress and interface debonded energy on the cracking stress and matrix crack evolution have been analyzed.
机译:利用能量平衡方法研究了单轴拉伸载荷下交叉陶瓷基复合材料的基体裂纹演变。当交叉层陶瓷基体复合材料受到拉伸载荷时,会发生90°层的横向开裂和0°层的基体开裂。交叉层压板的损坏状态可以分为五种模式。破裂模式3包括横向破裂,基体破裂和纤维/基质界面剥离。破裂模式5仅包含基质破裂和纤维/基质界面剥离。确定在两个存在的横向裂纹之间出现的模式3和5的裂纹应力。并确定了模式3的多矩阵裂纹演化。分析了层厚度,纤维体积分数,界面剪切应力和界面剥离能量对开裂应力和基体裂纹演变的影响。

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