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Numerical simulation of fatigue behavior of honeycomb sandwich panels

机译:蜂窝夹层面板疲劳行为的数值模拟

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In this study, based on Goodman stress correction algorithm, four point bending fatigue behavior of brazed steel honeycomb sandwich panels at room temperature is simulated using Fe-safe emulation module. The cyclic load was sinusoidal with a frequency f= 10 Hz. The residual life and security coefficient are given in the condition of design fatigue lifetime of 10~6 cycles. The results show that, in the local deformation, local maximum deformation occurs in the core wall under the load region, indicate that this region is the failure region of fatigue. And the residual life of the core wall in this region is less because of local stress concentration, the probability of failure becomes high, while the residual life in the region far away from the mid-span is high.
机译:在本研究中,基于Goodman应力校正算法,使用Fe-Safe仿真模块模拟室温下钎焊钢蜂窝夹层板的四点弯曲疲劳行为。循环载荷是频率f = 10Hz的正弦载荷。在10〜6周期的设计疲劳寿命的条件下给出了残余寿命和安全系数。结果表明,在局部变形中,在负载区域下的芯壁中发生局部最大变形,表明该区域是疲劳的故障区域。并且由于局部应力集中,该区域中芯壁的剩余寿命较小,失效的概率变高,而远离中间跨度的区域的残余寿命是高的。

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