脆性基复合材料裂纹挠度和侵彻准则

N. Pagano
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摘要

在这项工作中,我们将考虑控制单向脆性基复合材料(BMC)行为的三个最关键的机制,使它们显示出足够的强度和损伤容限(或韧性)的所需特性。由未涂层碳化硅纤维和热膨胀系数主要不同的两种不同玻璃基体制成的复合材料进行了制作和测试,以确定基体裂纹起裂应力(图1)、纤维断裂(图2)和界面断裂韧性的下限(图3)。此外,这些测试为检验之前导出的轴对称损伤模型(ADM)的质量提供了直接证据[1,2]。虽然没有观察到损伤容限,因为应力-应变曲线与破坏呈线性关系,但在最终破坏之前,一个稳定的(显然)全细胞矩阵裂纹系统(图1)已经形成。目前还不清楚基质裂缝是在进入纤维之前就停止了,还是已经穿透了纤维本身。
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Crack Deflection and Penetration Criteria for Brittle Matrix Composites
In this work, we will consider the three most crucial mechanisms that control the behavior of unidirectional brittle matrix composites (BMC) such that they display the desired characteristics of adequate strength and damage tolerance (or toughness). Composites made with uncoated silicon carbide fibers and two different glass matrices which differ principally in their thermal expansion coefficients were made and tested in order to determine matrix crack initiation stress (Fig. 1), fiber fracture (Fig. 2), and a lower bound interface fracture toughness (Fig. 3). Furthermore, these tests provide direct evidence to examine the quality of an axisymmetric damage model (ADM) derived earlier [1, 2]. Although there was no observed damage tolerance in that both stress-strain curves were linear to failure, a stable system of (apparently) full-cell matrix cracks (Fig. 1) develops prior to ultimate failure. It is not clear if the matrix cracks have arrested prior to entering the fiber or if they have penetrated the fiber itself.
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