一种有效的分析弹塑性问题的边界元法

本文提出了一组有效的边界元公式.该公式通过利用一个新的变量,使核函数仅具有lnr(r为源点和场点的距离)的较低阶奇异性,从而,在积分点的传统位移和应力公式的奇异性得到降低,且原公式中影响应力计算精度的边界层效应得到消除.同时,也避免了难于计算的参数C.将该方法应用到弹塑性分析中,数值分析结果表明该公式具有明显的优势.     

An effective boundary method for the analysis of elastoplastic problems

In this paper, a series of effective formulae of the boundary element method is presented. In these formulae, by using a new variable two kernels are only of the weaker singularity of Lnr (where r is the distance between a source point and a field point). Hence, the singularities in the conventional displacement formulation and stress formulation at internal points are reduced respectively so that the "boundary-layer" effect which strongly degenerates the accuracy of stress calculation by using original formulae is eliminated. Also the direct evaluation of coefficients C (boundary tensor), which are difficult to calculate, is avoided. This method is used in elastoplastic analysis. The results of the numerical investigation demonstrate the potential advantages of this method.     

涡流无损检测温度影响研究

增材制造是一种先进的金属制备方法，能够极大满足个性化的制造需求。制造过程中由于工艺原因可能会出现裂纹等典型缺陷。涡流无损检测对于增材制造结构件的裂纹缺陷是一种潜在的有效评价手段。在增材制造过程中，构件残余热会影响检测效果，需要开发抑制温度影响的涡流信号处理方法。基于以上背景，本研究开展了以下工作：(1)对涡流检测信号受温度影响的机理进行了详细分析，包括涡流检测信号温漂的影响因素以及这些因素随温度的变化规律。(2)基于数值计算验证了涡流检测信号的温漂规律。(3)搭建了涡流检测实验平台，通过该平台进行实验发现，待测导体温度越高缺陷信号越小。(4)针对自激自检探头信号温漂难题，设计了双探头差动补偿形式，开发了涡流信号间接差分信号处理方法。(5)使用上述差动补偿形式和信号处理方法，达到了减弱涡流信号漂移、提高涡流信号信噪比的目的。