137 resultados para cylinder wake


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A perturbation solution is obtained for the local stress-strain fields in an axially cracked cylindrical shell. The tenth-order differential equations are used that take into account the transverse shear deformation. The perturbation of a curvature parameter, λ, is employed, where . The stress intensity factors for finite size cylindrical shells subjected to bending and internal pressure are evaluated. Sufficient accuracy can be obtained without using fine mesh sizes in regions near the crack tip. Also analyzed are the influence of cylinder diameter and shearing stiffness on bulging.

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The mechanism of ductile damage caused by secondary void damage in the matrix around primary voids is studied by large strain, finite element analysis. A cylinder embedding an initially spherical void, a plane stress cell with a circular void and plane strain cell with a cylindrical or a flat void are analysed under different loading conditions. Secondary voids of smaller scale size nucleate in the strain hardening matrix, according to the requirements of some stress/strain criteria. Their growth and coalescence, handled by the empty element technique, demonstrate distinct mechanisms of damage as circumstances change. The macroscopic stress-strain curves are decomposed and illustrated in the form of the deviatoric and the volumetric parts. Concerning the stress response and the void growth prediction, comparisons are made between the present numerical results and those of previous authors. It is shown that loading condition, void growth history and void shape effect incorporated with the interaction between two generations of voids should be accounted for besides the void volume fraction.

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The problem of thermophoretic deposition of small particles onto cold surfaces is studied in two-dimensional and axisymmetric flow fields. The particle concentration equation is solved numerically together with the momentum and energy equations in the laminar boundary layer with variable density effect included. It is shown explicitly to what extent the particle concentration and deposition rate at the wall are influenced by the density variation effect for external flow past bodies. The general numerical procedure is given for two-dimensional and axisymmetric cases and is illustrated with examples of thermophoretic deposition of particles in flows past a cold cylinder and a sphere.

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In this paper, applying the direct variational approach of first-order approximation to the capillary instability problem for the eases of rotating liquid column, toroid and films on both sides of cylinder, we have obtained the necessary and sufficient conditions for motion stability of the "cylindrical coreliquid-liquid-cylindrical shell" systems. The results obtained before are found to be special cases of the present investigation. At the same time, we have explained physical essence of rotating instability and settled a few disputes in previous investigations.

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The stationary two-dimensional (x, z) near wakes behind a flat-based projectile which moves at a constant mesothermal speed (V∞) along a z-axis in a rarefied, fully ionized, plasma is studied using the wave model previously proposed by one of the authors (VCL). One-fluid theory is used to depict the free expansion of ambient plasma into the vacuum produced behind a fast-moving projectile. This nonstationary, one-dimensional (x, t) flow which is approximated by the K-dV equation can be transformed, through substitution, t=z/V∞, into a stationary two-dimensional (x, z) near wake flow seen by an observer moving with the body velocity (V∞). The initial value problem of the K-dV equation in (x, t) variables is solved by a specially devised numerical method. Comparisons of the present numerical solution for the asymptotically small and large times with available analytical solutions are made and found in satisfactory agreements.

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首先从涡脱落生成理论出发对钝体尾流控制方法进行了分类,并简单介绍r国内尾流控制研究情况.之后介绍r我们用窄条或小方柱取代小圆柱后,对Strykowsky和Sreenivasan控制方法的改进及其在高雷诺数下对圆柱和方柱尾流涡脱落的有效抑制情况,并探讨了控制件钝度对抑制效果的影响.第3部分用实验数据对各个涡脱落生成模型做了分析与检验,指出控制件方法的机理与改变钝体分离位置、减小钝体背压吸力、改变流动的腱向相关性、防止钝体两侧剪切层相互作用等无关,而与钝体近尾流速度剖面的局部修正及其稳定性的改变有关.最后简单介绍了控制件方法今后研究工作展望及其工程应用前景.

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针对轴形零件实际焊接加工中遇到的困难,利用现场总线、串口通信和GALIL运动控制卡实现了上位计算机对激光器、机器人以及旋转台等系统的同步控制,提出了集成化激光制造系统的多种控制工艺焊接方法。对轴形零件进行了各种激光焊接控制工艺的实验研究,证明了此控制系统可实现多种焊接控制工艺,可以满足轴形零件激光焊接中变速度、变功率、偏角度等各种工艺条件焊接的需求,为轴形零件实际激光焊接中遇到的焊接过程不稳定、首尾衔接处凹坑缺陷等难题的解决提供了新的方法。编程采用VC++面向对象工具加以实现。

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针对一阶畸变波Born近似模型,深入分析了湍流内外尺度和电子数密度脉动值对雷达散射截面的影响,并且给出了关于湍流外尺度的一个经验的,能被工程上较好使用的公式.在以上分析的基础上,计算了几种高程条件下再入小钝头锥体等离子尾迹的雷达散射截面,与已有实验结果进行了对比分析.分析和计算结果表明,湍流的外尺度和局部电子数密度值对雷达散射截面值影响较大;湍流内尺度变化的影响不大.

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再入飞行器湍流尾迹流场状况,直接系统到飞行器的雷达散射特性。对再入飞行器湍流尾迹等离子体场理论模型,试图通过湍流模式理论来表达,即使用k-ε-g模型方程来封闭平均化的全Navier-Stokes方程,从而准确获得流动平均场和脉动场住处。使用的N-S平均议程由质量加权平均过程产生,湍流模型方程也经过可压缩性能修正。真实气体效应重点考察空气处于局部热化学平衡状态。流动控制方程运用一个二阶TVD格式有限体积法求解。以一典型小钝锥体零攻角再入飞行为例,计算了在两高程(H = 40 km和H = 30 km)条件下的高超声速湍流尾迹流场。获得的尾迹流场参数与流动物理状况符合,并且湍流脉动参数与已有相应的实验结果定性一致,初步证实该方法合理。

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通过探讨高超声速再入湍流尾迹等离子体场中电磁波的散射机制,推导出在工程上描述湍流亚密等离子体雷达散射的一阶畸变波Born近似模型,分析了该模型在充分发展湍流尾迹等离子体场中的适用性,完成了适用于三维尾迹等离子体场的程序设计。以已有的湍流尾迹等离子体流场数据为基础,分析了再入尾迹湍流等离子体流动对雷达散射截面的影响。选取考察的几个有代表性的因素为:湍流模型、转捩过程、湍流尺度、电子组分脉动初始条件等。由结果可以看到,湍流转捩过程和湍流尺度对雷达散射截面值影响不大;电子组份脉动强度初始值影响较明显;湍流模型在特定条件下影响亦不大。

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对采用两种不同热处理工艺的钛合金TC4材料进行了Hopkinson拉伸实验、圆筒爆炸实验和数值仿真,从而确定了两种不同热处理工艺的优劣并通过微观分析揭示了钛合金TC4材料微观组织结构对内爆炸载荷下圆筒膨胀半径的影响.实验和数值分析表明:采用双重退火热处理工艺的钛合金TC4材料具有良好的动态力学性能.在相同的加载条件下,经此工艺处理的TC4圆筒在爆轰产物未泄漏之前有着充分的膨胀半径,而且也不容易形成绝热剪切破坏.同时,给出的依据高速摄影照片确定筒壳断裂点的方法是切实可行的,获得的断裂时间与数值分析结果吻合.

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研究了雷诺数Re=200,1000,线速度比α=0.5,2.0,4.0,强迫振荡频率fs=0.1~2.0情况下的旋转振荡圆柱绕流问题.通过基于非结构同位网格有限体积法对Navier-Stokes方程进行数值求解.对流项、扩散项和非恒定项的离散格式均具有二阶精度,利用SIMPLE算法处理压力-速度耦合.计算得到了作用力系数随不同控制参数的变化规律.通过对升力系数的频谱分析得到自然脱落频率和强迫振荡频率下的作用力振幅.通过对不同频率作用力幅值的分析,得到频率之间的竞争关系,进而定量地给出了不同尾迹涡脱落模式的分区图.

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以具有轴对称性质、端部带有半埋藏环形裂纹的厚壁圆筒为研究对象,通过对长厚壁圆筒内外环面均匀通入超强脉冲电流进行电磁热止裂。采用复变函数方法求解了脉冲放电瞬间裂纹尖端的温度场和热应力场。在一定的超强脉冲电流作用下,由于环形裂纹尖端的电流绕流热集中效应,裂尖温升超过了金属熔点,使裂尖处金属熔化在内部形成堆焊,钝化了裂尖,并且在裂纹前缘形成了热压应力,阻止了裂纹的扩展。在此基础上还讨论了在电载荷和机械载荷共同作用下裂纹前缘的应力场。

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通过数值求解三维不可压缩Navier-Stokes方程,研究了振荡圆柱绕流的旋涡不稳定性。研究表明,在一定的参数范围内,由于旋涡不稳定性,振荡流出由二维演化成三维流动,并沿圆柱轴向形成交错排列的三维涡结构。数值计算合理地预测了三维涡结构的空间失稳波长,并与实验测试值相符很好。文中还进一步研究了圆柱的受力特性,通过求解Morison方程,计算了圆柱的阻力和惯性力特性,其计算结果与已有的实验数据相吻合。

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利用Ghost Fluid方法(后面简称Ghost方法)和γ-model方法,在同样的时空离散精度条件下,对激波与柱形界面相互作用的二维可压缩流场进行了直接模拟,并与实验结果相比较.从模拟结果看,在短时间内, Ghost方法和γ-model方法模拟的结果与实验结果基本相同,两种方法均正确地模拟出界面的位置、激波的强度和速度.但随着时间的发展,具有较大数值耗散的γ-model方法的计算结果与实验差别越来越大;而数值耗散较小的Ghost方法能较为正确地模拟界面的运动.