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Fatigue crack propagation of through cracks in thin sheets under combined traction and bending stresses

机译:牵引和弯曲应力共同作用下薄板贯通裂纹的疲劳裂纹扩展

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Fatigue crack propagation tests of through cracks in 3 mm thick aluminium alloy 6013-T6 plates, under combined membrane and bending stresses were carried out. Five different values for the ratio of bending to membrane stresses, SB, were examined: 0, 0.55, 1.25, 1.8 and 2.23. Firstly, the results were elaborated by taking into account only the membrane stress and the front dimension of the crack for the evaluation of the stress intensity factor range. The results relevant to the lower SB values, evaluated in this mode, show good agreement with the results obtained when only the membrane stress was applied, while the results obtained at the higher SB values exhibit a remarkable increase in the crack propagation rate. The results were successively evaluated on the basis of tabular stress intensity factor solutions available in the literature; the agreement between the predicted and the experimental data occurs when mean values of stress intensity factor, rather than local values, were used at the back face of the plate, i.e., the face where the bending produces a compressive stress, to counteract the high gradient of stress intensity factor present in this area. [References: 11]
机译:在3mm厚的铝合金6013-T6板在复合膜和弯曲应力作用下进行了贯通裂纹的疲劳裂纹扩展试验。检查了弯曲与膜应力之比SB的五个不同值:0、0.55、1.25、1.8和2.23。首先,在评估应力强度因子范围时,仅考虑膜应力和裂纹的正面尺寸来详细阐述结果。在此模式下评估的与较低SB值相关的结果与仅施加膜应力时获得的结果良好吻合,而在较高SB值下获得的结果表明裂纹扩展速率显着提高。根据文献中提供的表格应力强度因子解,对结果进行了连续评估;当在板的背面(即弯曲产生压缩应力的面)使用应力强度因子的平均值而不是局部值时,会发生预测数据与实验数据之间的一致性,以抵消高梯度存在于该区域的应力强度因子。 [参考:11]

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