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Effects of R-ratio on the off-axis fatigue behavior of unidirectional hybrid GFRP AI laminates at room temperature

机译:R比对室温下单向混合GFRP AI层压板离轴疲劳行为的影响

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摘要

Effects of stress ratio on the off-axis fatigue behavior of the unidirectional fiber-metal hybrid GFRP A1 laminate (GLARE-2) at room temperature are studied. Constant amplitude fatigue tests at three kinds of stress ratios R = 0.4, 0.1 and -0.2 are performed on coupon specimens with different fiber orientations theta = 0 deg, 5 deg , 10 deg , 15 deg , 20 deg , 30 deg , 45 deg , 60 deg and 90 deg in the GFRP layers. It is observed that the fatigue life of GLARE-2 is extended by the increase in stress ratio for every fiber orientation. A linear relationship of the Goodman type can approximately be fitted to the constant fatigue life data for GLARE-2, regardless of the fiber orientations. The fatigue fracture of GLARE-2 is characterized by the fatigue failure of the GFRP layers for theta = 0-15 deg, while it is brought about by the fatigue failure of the aluminum-alloy layers for theta = 30-90 deg. For each of the two groups, a master S-N relationship can be identified by means of a modified fatigue strength ratio. A fatigue damage mechanics model that considers the effect of stress ratio is developed using a modified theoretical fatigue strength ratio based on the Tsai-Hill static failure criterion. It is demonstrated that the fatigue model can successfully be used for description of the off-axis fatigue behavior of GLARE-2 over a range of stress ratios.
机译:研究了应力比对单向纤维-金属混杂GFRP A1层压板(GLARE-2)在室温下的轴外疲劳行为的影响。对具有不同纤维取向theta = 0度,5度,10度,15度,20度,30度,45度,3种应力比R = 0.4、0.1和-0.2的恒定振幅疲劳测试GFRP层分别为60度和90度。可以观察到,GLARE-2的疲劳寿命因每种纤维取向的应力比的增加而延长。不论纤维取向如何,Goodman类型的线性关系都可以近似拟合GLARE-2的恒定疲劳寿命数据。 GLARE-2的疲劳断裂的特征是θ= 0-15度的GFRP层的疲劳破坏,而它是由θ= 30-90度的铝合金层的疲劳破坏造成的。对于两组中的每组,可以通过修改的疲劳强度比来确定主要的S-N关系。基于Tsai-Hill静态破坏准则,使用修正的理论疲劳强度比,开发了考虑应力比影响的疲劳损伤力学模型。结果表明,该疲劳模型可以成功地用于描述GLARE-2在一定应力比范围内的轴外疲劳行为。

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