多载荷结构极限分析的无搜索迭代算法

详细研究了结构极限分析的现有方法,在考虑多组独立变化载荷联合作用的情况下,结合传统的极限分析理论,提出了加载路径射线辐射求解法,并基于这种射线辐射状的加载路径,推导了多组载荷联合作用下结构塑性极限上限分析的数学规划格式,并编制了相应的有限元程序。文中的数值算例表明本文所提出的这种射线辐射状的加载路径是合理且有效的,同时采用无搜索数学规划方法能够很好的避免弹塑性分段逐步增量的复杂计算,克服规划中目标函数非线性所导致的困难。     

残余应力与拘束对GH4169合金疲劳及蠕变-疲劳裂纹扩展速率影响研究

为深入理解残余应力与拘束在疲劳载荷下的交互作用,以镍基高温合金GH4169为研究对象,选用紧凑拉伸(CT)试样,对不同拘束CT试样的上方施加不同大小的预加载荷从而在裂尖产生不同应力。将该应力作为残余应力,系统研究残余应力和拘束交互作用下GH4169合金的疲劳和蠕变–疲劳裂纹扩展速率。结果表明：随着裂尖残余压应力的增加,不同拘束下GH4169合金的疲劳和蠕变–疲劳裂纹扩展速率均降低。与低拘束试样相比,高拘束试样的疲劳和蠕变–疲劳裂纹扩展速率对残余应力的变化更加敏感,这主要与裂尖Mises应力和垂直于裂纹扩展方向的正应力有关。与疲劳裂纹扩展速率相比,蠕变-疲劳裂纹扩展速率对残余应力的变化更加敏感。     

Novel magnetorheological figuring of KDP crystal

A new process of magnetorheological figuring(MRF) based on the deliquescence theory is proposed to finish KDP crystals.A novel,non-aqueous,and abrasive-free magnetorheological(MR) fluid is explored,and polishing experiments are performed on a self-developed MRF machine.The removal mechanism is reckoned to be the result of a combination of dominant chemical etching and accessorial mechanical drag.The results indicate that the surface roughness of I plate KDP of 80 × 80(mm) polished by MRF is 1.2 nm(root mean square(RMS)),and the tool marks are completely removed.The surface accuracy by MRF is 0.035λ(RMS),and the low/middle-frequency errors are significantly corrected after MRF.