机翼构件不同载荷谱下的寿命反推

对飞机机翼构件在不同截荷谱下的宏、微观断裂特征进行了观察与分析，并结合载荷谱中的应力变化特点，对A飞机和B飞机翼构件在不同载荷谱下的裂纹扩展寿命进行反推。结果表明，载荷谱中不同的应力变化在失效构件断口上反映出不同的宏、微观断裂特征，采用断口定量分析技术可反推构件的疲劳寿命，并依此反推构件疲劳裂纹形核的先后顺序。     

基于局部应变能密度法的缺口多轴疲劳寿命评估

本文提出了包括实验和数值工作在内的综合分析,阐明了缺口行为对比例多轴疲劳寿命的影响。方法对45钢和45QT钢进行了考虑缺口半径和开口角的多轴疲劳试验,基于平均应变能量密度理论的多轴疲劳分析的分析和计算框架进行了研究,以处理能量梯度。结果显示,大量新的疲劳数据首先通过法向应力和剪应力进行汇总,然后通过凹口尖端周围受控体积中的局部应变能密度重新分析。结论缺口角度对比例载荷下多轴疲劳数据的影响较小,而缺口半径是影响疲劳寿命的主要因素。     

简支圆板在冲击荷载作用下的塑性动力响应分析

采用双剪应力强度理论求解了拉压异性材料简支圆板在中等脉冲荷载作用下的动力响应问题，得出了塑性动力极限荷载、内力场和速度场。讨论了静力许可条件和运动许可条件。利用本文的解还得出了简支圆板在静力荷载作用下的极限荷载、内力场和速度场。研究结果表明，材料的拉压强度比对动力解的影响要大于对静力解的影响，所以，根据材料的不同，选择合适的强度理论，对于更好地发挥材料的强度潜力具有重要的意义。     

Design of Fibre Reinforced Composite Structures Subjected to High Strain Rates Using Finite Element Analysis

A finite element analysis of fibre reinforced plastic tubes subjected to a dynamic internal pressure pulse is performed using the ABAQUS finite element program. The effects of strain rate on the ply properties, the nonlinearity of the stress-strain curves, failure and post-failure theories are incorporated in the analysis. The results of the analysis show good agreement with the experimental stress-strain and strain-time results for 45° and 65° Kevlar fibre reinforced epoxy (KRP) tubes.     

加载频率与应变比对10CrNi5Mo高强钢低周疲劳寿命的影响

通过对圆形横截面光滑试样进行轴向应变控制的低周疲劳试验,研究了加载频率与应变比对10CrNi5Mo高强钢疲劳寿命的影响。结果表明:在较低频率(0.05～0.1 Hz)范围内,频率对疲劳寿命的影响不明显,随着加载频率的增加(0.1～0.8 Hz),疲劳寿命显著提高,当加载频率增加到0.8 Hz时,疲劳寿命达到最大值,随着加载频率的继续增加(0.8～1.0 Hz),疲劳寿命反而有所下降;在最大应变不变条件下,随着应变比的增加(-1～-0.3),疲劳寿命平稳上升,当应变比增加到-0.30时,随着应变比的继续增加,材料的疲劳寿命急剧升高。研究结果为10CrNi5Mo高强钢的工程应用提供了依据。     

Theoretical Analysis on the Measurement Errors of Local 2D DIC: Part II Assessment of Strain Errors of the Local Smoothing Method–Approaching an Answer to the Overlap Question

In this paper, the strain error of subset‐based two‐dimensional digital image correlation (DIC) is theoretically derived. Analytical solutions are provided to estimate the strain error. A dimensionless factor is proposed, namely the overlap magnifier, which reveals the dependency of the strain error on the DIC regularisation parameters, that is, subset size, step size and strain window size. The derived equations are validated numerically and experimentally. The estimated random strain error is in good accordance with the experimental data. The proposed derivation can be readily extended to stereo DIC.