TRANSIENT TORSIONAL WAVE IN FINITE HOLLOW CYLINDER WITH INITIAL AXIAL STRESS

An analytical solution is obtained for transient torsional vibration of a finite hollow cylinder with initial axial stress. The cylinder is subjected to dynamic shearing stress at the internal surface and is fixed at the external surface. The basic equations are presented and the solution is obtained by means of Fourier series expansion technique and the separation of variables method. The effects of the initial stress on the natural frequencies and transient torsional responses are presented and discussed.     

采用“一次逐差法”处理实验数据的物理内涵

本文详细阐述了在物理实验中采用一次逐差(也称差数平均值)法处理数据的物理实质，及引用该法的过程和条件，说明了这一方法的采用完全是由实验过程所决定，是实验过程的必然延续．而不是由于该方法本身能避免“中间数据”不起作用这一数学特点．全文以我校开设的“拉伸法测定钢丝的弹性模量”为例进行详细全面的讨论．     

混合单调算子的两点拉伸型不动点定理

本文首次提出了混合单调算子不动点的两点拉伸型条件.同时,利用锥映象的不动点指数理论建立了一类特殊的两点拉伸型混合单调算子的不动点存在性定理,并将所得结论应用于带有超线性项的积分方程与微分方程上,得到了新的结论.因而在本质上推进了混合单调算子不动点问题的研究.     

泊松比对拉伸法测材料杨氏模量的影响

用拉伸法测杨氏模量较小的圆形材料杨氏模量实验时,伴随材料的拉长,其直径将明显减小.此时,实验必须考虑材料直径的变化.以拉伸法测圆形硅胶的杨氏模量为例,将材料直径的变化通过泊松比转为材料伸长量,实验结果表明引入泊松比所测杨氏模量精确度提高,不确定度减小.     

FeCoCrCuNi高熵合金裂纹及孔洞结构力学与微观构象演化机理的分子动力学模拟研究

本文采用分子动力学方法研究了FeCoCrCuNi高熵合金裂纹及孔洞模型结构在不同轴向拉伸应变速率下的力学与微观结构演化机理. 结果表明：应变速率越高FeCoCrCuNi裂纹结构对应更高的过冲应变和过冲应力,其主要原因是高拉伸速率会导致高强度的BCC结构及孪晶结构的生成,而BCC结构及孪晶结构的产生进而会抑制应力的下降,通过应力-应变曲线,可知FeCoCrCuNi裂纹模型在轴向应力作用下表现为塑性形变. 对于不同尺寸的孔洞FeCoCrCuNi裂纹模型的应力模拟与结构分析,可以得出：孔洞尺寸越大, FeCoCrCuNi裂纹结构对应的过冲应变和过冲应力越小,其主要原因是大尺寸的孔洞造成孔洞之间产生裂纹的,进而会影响这个材料的屈服应变和屈服强度.     

飞机的噪声环境及其结构的声振疲劳

本文简述了对某类机动飞机进行噪声环境测量及其数据归纳的方法;根据编制的噪声载荷谱和受载特点,选择适当的噪声源,进行声疲劳试验,考核飞机结构声疲劳特性,并对测量、试验结果进行分析,评定了几种抗声疲劳性能较高的结构形式。     

国产航空有机玻璃在冲击载荷下的热粘弹性力学响应

本文以鸟撞高速飞机风档问题为背景,对国产航空有机玻璃3~#PMMA在从准静载荷的应变率(10~(-4)S~(-1))直到冲击载荷的高应变率(10~3S~(-1))范围,和环境温度从-60℃到+100℃范围内的力学性能进行了系统的实验研究,并建立了相应的非线性热粘弹性本构方程。理论预示与实验结果符合。另外还对3~#PMMA低温及高应变率冲击脆化现象进行了讨论,发现与这一现象相一致,3~#PMMA在高应变率冲击条件下的玻璃化温度有明显的提高。     

Casson fluid flow and heat transfer over a nonlinearly stretching surface

A boundary layer analysis is presented for non-Newtonian fluid flow and heat transfer over a nonlinearly stretching surface. The Casson fluid model is used to characterize the non-Newtonian fluid behavior. By using suitable transformations, the governing partial differential equations corresponding to the momentum and energy equations are converted into non-linear ordinary differential equations. Numerical solutions of these equations are obtained with the shooting method. The effect of increasing Casson parameter is to suppress the velocity field. However the temperature is enhanced with the increasing Casson parameter.     

The effect of intragranular microstress in A1203-SiC nanocomposites

A theoretical model is established to investigate the intragranular particle residual stress in A1203-SiC nanocom-posites. Using this model, we calculate the average compressive stress on the A1203 grain boundary （GB） and the average tensile stress within A1203 grains caused by SiC nanoparticles. The normal compressive stress strengthens the GB, and the average tensile stress weakens the grains. The model gives a reasonable interpretation of the strength changes of A1203-SiC nanocomposites with the number of SiC particles.