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Temperature-dependent monotonic and fatigue bending strengths of adhesively bonded aluminum honeycomb sandwich beams

机译:铝蜂窝夹芯梁的温度相关的单调和疲劳弯曲强度

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The monotonic and fatigue strengths of adhesively bonded aluminum honeycomb sandwich beams subjected to four-point bending were investigated at temperatures ranging from -25 to 75 ℃. Experimental results showed that the ultimate loads in the monotonic tests and fatigue strengths in the fatigue tests decrease as temperature increases, and the failure mode changes from local indentation to debonding at the skin/core interfaces. An analytical procedure based on the temperature-dependent monotonic strengths of face/core materials and simple adhesively bonded specimens were used and accurately predicted the ultimate applied loads in the monotonic tests by comparing the theoretical limit loads corresponding to several failure modes, i.e., face failure, local indentation, core shear failure, and face/core debonding modes. Furthermore, by modifying the monotonic analytical procedure and incorporating the temperature-dependent S-N curves of the face/core materials and the simple adhesively bonded specimens, the fatigue life of the sandwich beams could be predicted by comparing the estimated fatigue lives corresponding to various failure modes. Comparing the evaluated ultimate loads and fatigue lives with the observed data confirmed that the good prediction performance was obtained both in the monotonic and fatigue analyses.
机译:研究了-25℃至75℃温度范围内四点弯曲粘结铝蜂窝夹芯梁的单调强度和疲劳强度。实验结果表明,单调试验的极限载荷和疲劳试验的疲劳强度随着温度的升高而降低,并且失效模式从局部压痕改变为表皮/核心界面的脱粘。使用了基于面/芯材料随温度变化的单调强度和简单的粘合样本的分析程序,通过比较对应于几种破坏模式(即面破坏)的理论极限载荷,准确预测了单调测试中的最终施加载荷,局部压痕,岩心剪切破坏和面/岩心脱胶模式。此外,通过修改单调分析程序并结合面/芯材料和简单的粘结样本的温度相关SN曲线,可以通过比较与各种失效模式对应的估计疲劳寿命来预测夹层梁的疲劳寿命。 。将评估的极限载荷和疲劳寿命与观察到的数据进行比较,证实了在单调和疲劳分析中均获得了良好的预测性能。

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