Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion

D. Rozumek, S. Faszynka
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引用次数: 13

Abstract

The paper presents the results of tests on the fatigue crack growth for a constant moment amplitude under combined bending with torsion in the aluminium alloy AW-2017A-T4. The tests were performed under different values of the load ratio R. Plane specimens with stress concentrators in form of the external one-sided sharp notch were tested. A non-uniform fatigue cracks growth on both lateral surfaces of specimens was observed during experimental tests. Fatigue cracks were developing in the specimens in two stages; quarter-elliptic edge cracks were observed at the beginning, then evolving into through cracks.
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2017A-T4合金比例弯曲与扭转作用下的疲劳裂纹扩展
本文介绍了AW-2017A-T4铝合金在弯曲和扭转联合作用下的恒矩幅疲劳裂纹扩展试验结果。在不同的载荷比r值下进行了试验。对平面试样进行了应力集中器的试验,其形式为外侧边尖缺口。在试验过程中,观察到试样两侧表面出现不均匀的疲劳裂纹扩展。试件的疲劳裂纹发展分为两个阶段;首先观察到四分之一椭圆边缘裂纹,然后演变为透裂纹。
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