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FATIGUE IN SPRUCE LUMBER UNDER COMPRESSION PARALLEL TO GRAIN

机译:压缩下云带的疲劳平行于谷物

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The low-cycle fatigue (LCF) behaviour of spruce lumber in compression parallel to grain was investigated. Specimens were relatively knotty and grouped according to knot area. Tests employed a sinusoidal waveform, peak load of 0.9 short-term crushing load (F_(ult)), valley load of 0.1F_(ult), and loading frequency of 0.5Hz. The F_(ult) for each fatigue specimen was estimated based on behaviour of a matched control group. Fatigue tests were stopped if there had been no failure within 10 minutes (300 load cycles). Specimens that failed did so mainly due to formation of creases in clear wood regions adjacent to knots. Both cyclic creep deformation (CCD) and cyclic accumulated deformation (CAD) increased as load cycling progressed. Energy dissipation (hysteresis loop area H) was relatively stable except during initial load cycles and near to failure. Beyond the first 5% of the normalised fatigue life, residual stiffness reduced due to load cycling. Residual stiffness was found to be a better damage index than CCD, CAD or H.
机译:研究了云端云带在平行于晶粒的压缩中的低周期疲劳(LCF)行为。样品相对齐全,并根据结区域进行分组。试验采用正弦波形,峰值负荷为0.9短期破碎负荷(F_(ULT)),谷载荷0.1F_(ULT),加载频率为0.5Hz。基于匹配对照组的行为估计了每种疲劳样本的F_(ULT)。如果在10分钟内没有发生故障(300次负载循环),则停止疲劳试验。失败的标本如此,主要是由于透明木地区的折痕形成。随着负载循环的进展,循环蠕变变形(CCD)和循环累积变形(CAD)都增加了。除初始载荷循环和近发生故障近,除了在初始载荷周期之外的能量耗散(滞后环H)相对稳定。除了归一化疲劳寿命的前5%之外,由于负荷循环,残留刚度降低。发现残余刚度是比CCD,CAD或H更好的损伤指数。

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