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Elastic shielding during fatigue-crack growth of titanium matrix composites

机译:钛基复合材料疲劳裂纹扩展过程中的弹性屏蔽

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The role of elastic shielding inreducing the local stress intensity factor(SIF)range during fatigue crack growth (FCG) has beeninvestigated using several single-ply compositeswith significantly different interfacial characteristics. The specimen geometrynecessitated the fatigue crack to initially growthrough a monolithic matrix region beforeimpinging on a set of longitudinally orientedfibers. This facilitated the assessment of thecrack shielding phenomenon from two regions: theregion where the crack interacted with the firstfiber, and at high stress levels when nonbridgingconditions prevailed in the fibrous region. Theextent of shielding was nearly identical in thetwo measurements for a given composite system.However, the shielding contribution was found todepend on the interface bond strength; theinterface with the highest bond strength providedthe largest degree of crack retardation in bothcases. A preliminary assessment of this dependencyhas been provided. The implications of using thecorrect shielding factor on both fiber strengthand life prediction are also discussed.
机译:研究了几种具有明显不同界面特性的单层复合材料,研究了弹性屏蔽在疲劳裂纹扩展(FCG)过程中减少局部应力强度因子(SIF)范围的作用。试样的几何形状需要使疲劳裂纹首先开始穿过整体的基体区域,然后再冲击一组纵向取向的纤维。这有助于从两个区域评估裂纹屏蔽现象:裂纹与第一纤维相互作用的区域,以及在纤维区域中普遍存在非桥接条件时处于高应力水平的区域。对于给定的复合材料体系,两次测量的屏蔽程度几乎相同。但是,发现屏蔽作用取决于界面粘结强度。在两种情况下,具有最高粘结强度的界面都提供了最大程度的裂纹延迟。已对此依赖性进行了初步评估。还讨论了使用正确的屏蔽系数对纤维强度和寿命预测的影响。

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