显微组织对Al-Mg-Si合金断裂行为的影响

 <正> The hardness, tensile strength and fatigue properties of an Al-Mg-Si alloy were measured in this paper. The microstructures were observed using a transmission electron microscope. The tensile and fatigue fractures were studied by scanning electron microscopy. The results show that the microstructure affects the fracture behavior of the alloy markedly. The alloy exhibits dimpled fracture in UA and OA conditions, and mixed fracture with dimples and intergranular rupture in PA condition. The fatigue cracks were developed with the features of the alloy in UA condition. The cracks were developed with the second stage mode and the striations could be seen on the surface of the fractures for the alloy in PA and OA conditions. But the intergranular fracture and facets could also be seen in the crack initiation area at these conditions.     

DO 28非线性多点模型的建立及其参数估计

 本文建立了DO 28试验机的非线性六自由度多点数学模型。该模型考虑了飞机运动的高度非线性,螺旋桨、机翼、尾翼空气动力特性,改进的推力计算,风场干扰以及飞行试验数据一致性检验和校正。与一点模型相比,该模型能更准确地描述飞机的运动,更适合飞机的参数估计。     

喷丸产生的残余拉应力场及材料的内部疲劳极限

 本文采用大型弹塑性分析有限元程序ADINA-84计算了40Cr钢9种规范的喷丸残余应力场,获得了残余拉应力场的计算表达式,并根据疲劳试验结果,提出了内部疲劳极限概念及喷丸强化的内部疲劳极限理论。     

腐蚀电场平面问题边界元法研究

 研究腐蚀电场平面问题的边界元理论和分析方法。首先,详细论述腐蚀电场平面问题的边界元理论。其次,针对电极极化曲线的非线性特性,提出一个求解含非线性边界条件的边界元问题的迭代解法。最后,按本文所述理论和方法,具体计算了某些电偶腐蚀电场的电位与电流密度分布,并与有关实驻结果比较,发现二者相符甚好。     

具有销钉承载孔的复合材料层合板的接触应力分析

 <正> 本文采用以弹性接触理论为基础的有限元混合法分析具有销钉承载孔的复合材料层合板的接触应力,并讨论了销钉的材料性质、层合板铺设方式以及销钉与承载孔边摩擦和公差诸因素对层合板承载孔边接触内力和应力分布与大小的影响。     

含孔边裂纹有限大板的解析变分解法

 本文利用复变函数方法导出了含孔边单侧裂纹有限大板应力与位移的全场表达式,满足所有基本方程、裂纹表面边界条件与复连通域位移单值条件。应用变分原理满足其余的边界条件并由此求解应力强度因子与应力集中系数。在变分方程中,只存在线积分,没有面积分。故本方法收敛迅速、节省机时。     

低信噪比情况下识别模态参数的时域平均方法

 <正> 1.引官 模态参数识别方法在应用中需要解决的一个重要问题是观测噪声的干扰问题。为了有效地抑制观测噪声的影响,各种时域参数识别方法普遍引入了估计方法,以ITDM为代表的利用脉冲响应包括对脉冲激励的响应和脉冲响应函数)识别模态参数的识别方法还引入了噪声模态     

涡量场测量

 <正> The space .distributions of vorticity were measured by using a vorticimctcr (vorti-city probe) in the field induced by a vortex shedding from the wing-tip of a rectangular wing under different angles of attack. The results show that the vorticimetcr having the advantages of high sensitivity, simpler calibration process and easiness to use, is capable of measuring the vorticity directly, and finding out the center trace of the vortex core exactly. Through the measurements, a counter rotating vortex with a center strength of 1/17 to that of the main wing-tip vortex existing nearby is discovered. The center vorticity would decay substantially as the main wing-tip vertex moves down-stream. For instance, the peak vorticity at x = 2.5c (c, the chord length) will decay to about 25% of that at x = 0.1c, while its scale remains almost unchanged. At the cross-section x = 0.1c, the scale of the wing-tip vortex was about 0.2c spanwisc and-0.18c along the longtudinal direction. Finally, the strengths of a pair of in     

升阶谱技术在时域问题中的应用

 本文把升阶谱技术应用于时间域,建立了一种高精度的逐步积分法。它能自由地升高阶次,以满足预定的精度要求。对于一些工程问题是一种很有效的方法。Wilson-θ法及孙焕纯的改进θ法都是本文方法的特例。     

振动试验和颤振分析的一体化——颤振实时分析系统

 <正> “颤振实时分析系统”是航空航天工业部振动环境课题组于1985年～1988年期间组织研制的一项课题,它是参考80年代美国波音公司的振动和颤振分析方法,吸收国内最新研究成果而发展的一套计算机辅助工程软件。