圆柱浮体的平衡姿态及其稳定性

浮心相当于浮体的支承点,其位置随物体的姿态而变化;物体稳定平衡时重心与浮心的距离达到极小。圆柱浮体有2~5个平衡位置,其中相间的1~2个稳定,其姿态与比重和长径比相关,在系统参数变化时可能突变。     

基于波尔兹曼方法研究幂律流体的椭圆柱绕流

基于格子波尔兹曼方法(lattice Boltzmann method) 和幂律流体本构方程, 建立二维流动模型, 将充分发展的速度分布与理论解进行对比, 吻合良好. 对幂律流体的圆柱绕流进行模拟, 采用了反弹格式的无滑移圆柱边界, 并使用应力积分法计算阻力系数, 分析了稳态圆柱绕流时, 阻力系数随幂律指数n 以及雷诺数Re 的变化规律. 分析了椭圆横轴/纵轴长度比和幂律指数n, 对压力系数Cp 和黏度系数Cv 的影响. 得到的变化规律与有限元方法规律一致, 验证了格子波尔兹曼模型的可行性.     

内部爆炸作用下多层钢筒的动态响应

为评估内部爆炸作用下多层钢筒结构的防护效果,考察多层钢筒结构动态响应和变形吸能特征,采用两端开口、总厚度为50 mm的4层圆柱形Q345钢筒,在8.90~18.18 kg TNT药量下进行爆炸实验,并在容器外壁进行应变电测。实验后钢筒结构爆心局部发生塑性变形,内层钢筒变形最大,但未发生破坏。根据研究得到初步认识：采用爆心单位环面变形吸能的设计方法,可以较好地预估给定药量下所需钢筒的厚度;不同药量下,轴向距离超过多层钢筒结构的1/4内径后,其外壁环向变形峰值约减小为爆心截面环向应变峰值的1/2。

     

泡沫铝内衬对抗内部爆炸钢筒变形的影响

为提高承受内部爆炸载荷钢筒的抗爆性能,研究了泡沫铝内衬对钢筒变形的影响。首先通过对比实验,发现在本文的实验条件下,泡沫铝内衬导致钢筒变形增大,甚至发生了严重的破坏;进而建立有限元模型,研究了钢筒变形随爆炸当量、泡沫铝内衬厚度的变化机理和规律。结果表明,添加足够厚度的泡沫铝内衬能够减小钢筒变形,但泡沫铝厚度不足时,则可能起到相反的效果。对于固定尺寸的含泡沫铝内衬钢筒,随着爆炸当量增加,泡沫铝内衬对钢筒塑性变形的影响主要包含3种模式。模式1,泡沫铝可通过塑性变形吸收爆炸载荷,从而减小钢筒变形。模式2,泡沫铝内衬导致钢筒承受的载荷强度增大,钢筒塑性变形增大。模式3,泡沫铝对载荷强度的影响可忽略,泡沫铝通过增大结构质量减小钢筒塑性变形。

     

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.     

标准圆筒试验技术与数据处理方法研究

 对标准圆筒试验技术与数据处理方法进行了深入研究,在狭缝扫描实验中建立了新型、高效的照明技术、底片判读方法以及数据处理方法,得到了精度高、信息丰富的圆筒壁质点上的位移、速度、加速度和比动能结果。同时,通过VISAR技术直接测量了圆筒外表面径向膨胀速度-时间曲线,进而积分得到位移-时间曲线,与狭缝扫描结果相互印证和补充,进一步提高了测试可靠性。     

The efect of the couple stress parameter and Prandtl number on the transient natural convection flow over a vertical cylinder

An analysis is performed to study transient free convective boundary layer flow of a couple stress fluid over a vertical cylinder, in the absence of body couples. The solution of the time-dependent non-linear and coupled governing equations is carried out with the aid of an unconditionally stable Crank–Nicolson type of numerical scheme. Numerical results for the steady-state velocity, temperature as well as the time histories of the skin-friction coefcient and Nusselt number are presented graphically and discussed. It is seen that for all flow variables as the couple stress control parameter, Co, is amplified, the time required for reaching the temporal maximum increases but the steady-state decreases.     

Exact solution of functionally graded thick cylinder with finite length under longitudinally non-uniform pressure

Elastic analysis of a functionally graded thick-walled cylindrical pressure vessel is analytically studied in the present research. Gradation is considered for all mechanical properties along the thickness direction based on a power function. The constitutive relations are developed in the general cylindrical coordinate system for an axisymmetric pressurized cylinder. For simulation of these two deformation components, first order shear deformation theory is considered. The FG cylinder is subjected to longitudinally non-uniform pressure along the length of the cylinder. The present problem is applicable for simulation of non-uniform pressurized cylinder by fluids or gases.     

Validation of a novel very large eddy simulation method for simulation of turbulent separated flow

The paper describes the validation of a newly developed very LES (VLES) method for the simulation of turbulent separated flow. The new VLES method is a unified simulation approach that can change seamlessly from Reynolds‐averaged Navier–Stokes to DNS depending on the numerical resolution. Four complex test cases are selected to validate the performance of the new method, that is, the flow past a square cylinder at Re = 3000 confined in a channel (with a blockage ratio of 20%), the turbulent flow over a circular cylinder at Re = 3900 as well as Re = 140,000, and a turbulent backward‐facing step flow with a thick incoming boundary layer at Re = 40,000. The simulation results are compared with available experimental, LES, and detached eddy simulation‐type results. The new VLES model performs well overall, and the predictions are satisfactory compared with previous experimental and numerical results. It is observed that the new VLES method is quite efficient for the turbulent flow simulations; that is, good predictions can be obtained using a quite coarse mesh compared with the previous LES method. Discussions of the implementation of the present VLES modeling are also conducted on the basis of the simulations of turbulent channel flow up to high Reynolds number of Re_τ = 4000. The efficiency of the present VLES modeling is also observed in the channel flow simulation. From a practical point of view, this new method has considerable potential for more complex turbulent flow simulations at relative high Reynolds numbers. Copyright © 2013 John Wiley & Sons, Ltd.     

A ghost-cell immersed boundary method for large-eddy simulations of compressible turbulent flows

A methodology to perform a ghost-cell-based immersed boundary method (GCIBM) is presented for simulating compressible turbulent flows around complex geometries. In this method, the boundary condition on the immersed boundary is enforced through the use of ‘ghost cells’ that are located inside the solid body. The computations of variables on these ghost cells are achieved using linear interpolation schemes. The validity and applicability of the proposed method is verified using a three-dimensional (3D) flow over a circular cylinder, and a large-eddy simulation of fully developed 3D turbulent flow in a channel with a wavy surface. The results agree well with the previous numerical and experimental results, given that the grid resolution is reasonably fine. To demonstrate the capability of the method for higher Mach numbers, supersonic turbulent flow over a circular cylinder is presented. While more work still needs to be done to demonstrate higher robustness and accuracy, the present work provides interesting insights using the GCIBM for the compressible flows.