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1.
Normal and radial displacements of a shallow thin sheil of revolution are related by theoretical considerations. Radial displacements are calculated from slope measurements on the generatrices of the initial shell surface (before loading) and of the final shell surface (after loading). Membrane and bending stresses over the entire shell surface are then computed from the measured slope values and the calculated radial displacements. A measuring technique is developed which is especially suitable for shallow shells enclosed in small spaces. It consists mainly of making a cast of the initial and final shell surface using an epoxy platic. The disklike cast is cut along its diameter. The slope values are measured optically along the line which is formed by the intersection of the cutting plane with the deflection surface. The method is applied to a shallow thin shell of revolution in contact with a concentric piston and to a clamped circular plate, both experiencing large axisymmetric deflection.  相似文献   

2.
Experimental techniques are developed to study and measure the shear-wave velocity in an aluminum cylindrical shell subjected to a radial impact. The radial impact is obtained by exploding an electrical detonator inserted in plastic plugs mounted on the end of the shell. Strain gages, mounted on the outside surface of the shell at various axial locations, are used to obtain oscilloscope traces from which the shear-wave velocity can be calculated.  相似文献   

3.
A postbuckling analysis is presented for a shear deformable functionally graded cylindrical shell of finite length subjected to combined axial and radial loads in thermal environments. Heat conduction and temperature-dependent material properties are both taken into account. The temperature field considered is assumed to be a uniform distribution over the shell surface and varied in the thickness direction only. Material properties are assumed to be temperature-dependent, and graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents. The formulations are based on a higher order shear deformation shell theory with von Kármán–Donnell-type of kinematic nonlinearity. A boundary layer theory of shell buckling, which includes the effects of nonlinear prebuckling deformations, large deflections in the postbuckling range, and initial geometric imperfections of the shell, is extended to the case of functionally graded cylindrical shells. A singular perturbation technique is employed to determine the interactive buckling loads and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling response of perfect and imperfect cylindrical shells with two constituent materials subjected to combined axial and radial mechanical loads and under different sets of thermal environments. The results reveal that the temperature field and volume fraction distribution have a significant effect on the postbuckling behavior, but they have a small effect on the imperfection sensitivity of the functionally graded shell.  相似文献   

4.
This paper presents a technique for measuring deflections in cylinders. It is based on the Ligtenberg moiré technique which produces fringes that are contours of surface slope. To use the technique in measuring slopes in a cylinder surface, the optical system is modified so that the cylindrical coordinates of the test piece are transformed to a flat polar plot for photographing.  相似文献   

5.
薄壁圆柱壳流体冲击振动响应是一个复杂的流固耦合(FSI)动力学问题,对于薄壳状态监测与缺陷识别具有重要意义。基于Flügge壳体应力理论,得到壳体运动的高阶偏微分方程组(PDE),利用波传播方法获得圆柱壳系统振动响应。将壳体周围流体定义为理想声学介质,通过亥姆霍兹方程描述声压场,得到流固耦合条件下的薄壁圆柱壳受迫振动响应演变规律。针对薄壳裂纹损伤识别问题,基于断裂力学理论建立局部柔度矩阵,结合呼吸型线弹簧模型(LSM),构造裂纹附近应力及位移连续条件,获得含裂纹损伤充液圆柱壳的振动响应,进而给出一种基于振动能量流的裂纹损伤识别方法。研究结果表明:充液圆柱壳耦合系统在非线性激励下,位移响应在沿轴向、周向和径向的传播特性差异明显;裂纹的存在会导致结构局部柔度的降低和耦合系统固有频率下降;归一化输入功率流能够有效地对充液圆柱壳耦合系统进行结构裂纹损伤识别。研究结果可为充液薄壳振动响应方面的研究提供有益参考,也可为流固耦合条件下的结构裂纹损伤识别方面提供技术支持。  相似文献   

6.
In the traditional continuum mechanics, the effects of surface free energy are generally ignored. However, this cannot be the case for nanostructures because of their high surface to volume ratio; surface energy plays an important role in the mechanical responses. In the present study, the nonlinear buckling and postbuckling characteristics of cylindrical nanoshells subjected to combined axial and radial compressions are investigated in the presence of surface energy effects. To this end, Gurtin–Murdoch elasticity theory is implemented into the classical first-order shear deformation shell theory to develop an efficient size-dependent shell model incorporating surface free energy effects. Subsequently, a boundary layer theory is employed including surface effects in conjunction with the nonlinear prebuckling deformations, the large postbuckling deflections and the initial geometric imperfection. Finally, a solution methodology based on a two-stepped singular perturbation technique is utilized to obtain the size-dependent critical buckling loads and equilibrium postbuckling paths corresponding to the both axial dominated and radial dominated loading cases. It is observed that for the both axial dominated and radial dominated loading cases, surface free energy effects cause to increase the both critical buckling load and critical end-shortening of shear deformable nanoshell made of silicon.  相似文献   

7.
本文从三维弹性理论出发,用特征函数法研究多层横观各向同性圆柱壳的轴对称问题.把位移和应力分量的齐次解表达成特征函数展开式,并把特解部分用Fourier级数表示.以多层圆柱壳的内、外柱面作为齐次边界,同时考虑层间的连续条件,推导出问题的特征方程并用Muller法求解.文中运用传递矩阵技术处理多层问题,并用边界型最小二乘配点法处理端部边界条件.作为实例,对双层圆柱壳作了数值计算.  相似文献   

8.
张会杰  唐志平  李丹 《实验力学》2009,24(6):525-531
对不同几何尺寸和边界约束条件的TiNi合金圆柱壳进行了准静态径向压缩实验研究,利用数字摄像和图像处理技术得到了不同位置柱壳的变形特征和应变分布,结果表明,在柱壳表面受压处先出现相变铰,随着名义应变的增大,相变铰将发展成相变铰区;在柱壳表面受拉处出现相变铰,但此处材料先进入马氏体相.当径厚比和边界约束不变时,随着名义应变的增大,柱壳的耗能率和比能不断增加.当名义应变不变时,柱壳的耗能率和比能随边界约束个数的增多而增加,吸能效果更好,随径厚比的增加而减小,吸能效率下降.  相似文献   

9.
We analyze the steady-state response of a functionally graded thick cylindrical shell subjected to thermal and mechanical loads. The functionally graded shell is simply supported at the edges and it is assumed to have an arbitrary variation of material properties in the radial direction. The three-dimensional steady-state heat conduction and thermoelasticity equations, simplified to the case of generalized plane strain deformations in the axial direction, are solved analytically. Suitable temperature and displacement functions that identically satisfy the boundary conditions at the simply supported edges are used to reduce the thermoelastic equilibrium equations to a set of coupled ordinary differential equations with variable coefficients, which are then solved by the power series method. In the present formulation, the cylindrical shell is assumed to be made of an orthotropic material, although the analytical solution is also valid for isotropic materials. Results are presented for two-constituent isotropic and fiber-reinforced functionally graded shells that have a smooth variation of material volume fractions, and/or in-plane fiber orientations, through the radial direction. The cylindrical shells are also analyzed using the Flügge and the Donnell shell theories. Displacements and stresses from the shell theories are compared with the three-dimensional exact solution to delineate the effects of transverse shear deformation, shell thickness and angular span.  相似文献   

10.
采用多普勒光纤探针测速技术(Doppler pins system,DPS,又称全光纤位移干涉测速技术)和高速摄影技术,研究装配垫片对金属柱壳膨胀断裂的影响,获得了有无垫片对应柱壳外表面位置的速度曲线和垫片对柱壳膨胀断裂影响明显的高速摄影图像。实验结果表明:与无垫片区域相比,垫片区域的柱壳外表面经历了先凸起后内凹的过程,导致垫片对应柱壳的径向运动位移发生反复错位,最终低于无垫片区域约0.34 mm,该位移差可能导致柱壳发生径向剪切断裂;实验结果还表明,在垫片与间隙交界处两侧(沿垫片方向约7.5°、沿间隙方向约9°)处各增加了一条裂纹,该断裂模式既不同于环向拉伸断裂,也不同于45°的剪切断裂,而是由垫片/间隙边界产生的两束稀疏应力波传到柱壳外表面引起的扰动影响所致,这个新的断裂模式与柱壳材料的动态力学性能密切相关。数值模拟结果表明,装配垫片对柱壳断裂机制影响不仅包含该处附加的质量效应,还应考虑炸药通过垫片后作用在柱壳上的冲击加载幅值变化、冲击加载时序与其他部位不同步的差异,以及垫片/间隙交界处引起的表面波传播对柱壳断裂模式的后续发展行为的影响。  相似文献   

11.
Hong-Liang Dai  Ting Dai 《Meccanica》2014,49(5):1069-1081
An analytic study for thermoelastic bending of a functionally graded material (FGM) cylindrical shell subjected to a uniform transverse mechanical load and non-uniform thermal loads is presented. Based on the classical linear shell theory, the equations with the radial deflection and horizontal displacement are derived out. An arbitrary material property of the FGM cylindrical shell is assumed to vary through the thickness of the cylindrical shell, and exact solution of the problem is obtained by using an analytic method. For the FGM cylindrical shell with fixed and simply supported boundary conditions, the effects of mechanical load, thermal load and the power law exponent on the deformation of the FGM cylindrical shell are analyzed and discussed.  相似文献   

12.
Analysis of laminated piezoelectric cylindrical shells   总被引:2,自引:0,他引:2  
A new method is developed for three-dimensional stress analysis of laminated piezoelectric cylindrical shell with simple support. The shell can be subjected to various applied loadings, including distributed body force, inner and outer surface traction and potential. Each layer of the shell can be piezoelectric or elastic/dielectric, with perfect bonding assumed between each interface. The governing equations are solved by the state-space technique. Numerical results are presented to show the sensing and actuating effects of three-layered piezoelectric cylindrical shell. The project supported by the National Natural Science Foundation of China (19572027)  相似文献   

13.
The effects of the curvature radius of a cylindrical shell on stress intensity factors are investigated in circumferential (inner and outer) semielliptical surface cracks in a cylindrical shell. What is new in this paper is to have given: (1) The stress intensity factors for surface cracks in a cylindircal shell are determined by photoelastic technique. (2) By a special method photoelastic slices are handled for obtaining a clear caustic curve, and the stress intensity factors for surface cracks in a cylindrical shell are determined by the caustic method. (3) An approximate equation of curvature correction factor Fc is proposed. (4) Effects of the curvature radius R of a cylindrical shell on the stress intensity factors of surface cracks are obtained. The results of this paper are in fair agreement with already existing analytical results. The approximate equation of curvature correction factor Fc can be widely used for engineering purposes.  相似文献   

14.
针对内爆炸载荷下膨胀态金属柱壳的回收问题,设计了冻结回收试验方法,实现了起爆后不同时刻金属柱壳的冻结回收。基于一体式壳体提出了3种改进结构,并分别对4种柱壳结构在内爆载荷下的膨胀断裂过程进行数值模拟。结果表明,两段式结构最有利于减小非起爆端对预期回收中间段壳体的影响。根据选定的最优壳体结构和金属柱壳在起爆后不同时刻的膨胀外形特征,设计与之匹配的冻结回收装置并进行冻结回收试验。试验结果表明,设计的冻结回收试验方法可以实现膨胀态金属柱壳的回收,回收壳体的轴向和径向尺寸与设计理想值符合较好,整体误差可控制在10%以内。  相似文献   

15.
The model introduced in Part I of the present study is extended to take into account a flowing fluid, a mean radial pressure and initial pre-stress in circular cylindrical shells. The axial flow can be external, internal or annular and is described by the potential theory for inviscid and incompressible fluid. The computer program DIVA has been developed. It takes into account all the following complicating effects on the vibrations of circular cylindrical shells: (i) nonuniform boundary conditions around the shell edges including elastic boundary conditions; (ii) fluid–structure interaction including both flowing and quiescent fluids; (iii) internal, external and annular fluids; (iv) effect of a mean radial pressure and initial pre-stress; (v) elastic bed of partial extension in circumferential and longitudinal directions; (vi) intermediate constraints; (vii) added masses. It can be considered the most complete computer program specifically dedicated to dynamics of circular cylindrical shells. The Flügge theory of shells is used to describe the shell deformations. The system has been proved to be conservative for any combination of boundary conditions with restrained displacement at the shell ends. Numerical results show that shells clamped at the upstream end and simply supported at the downstream end have a larger critical velocity than simply supported shells, solving the paradox of Horáček and Zolotarev.  相似文献   

16.
利用二级轻气炮加载,进行了球状2A12铝弹丸垂直撞击圆柱壳自由梁实验。并进行了弹丸速度、圆柱壳直径和壁厚等因素对穿孔直径影响的数值模拟,数值模拟结果和实验结果基本吻合。通过量纲分析和数值模拟结合,推导了穿孔直径与相关影响参数的经验关系式。研究结果表明:当圆柱壳直径和厚度不变时,高速撞击产生的穿孔直径在径向和轴向都随着弹丸速度增大而增大;当弹丸速度和圆柱壳厚度不变时,高速撞击产生的穿孔直径随着圆柱壳自由梁直径的增大而减小;当弹丸速度和圆柱壳直径不变时,穿孔直径随着圆柱壳厚度的增大而减小。  相似文献   

17.
Two methods of holographic interferometry were applied to measure the displacements of the surface of a cylindrical shell clamped at both ends and subjected to a single radial load. In the first method the multiple-hologram technique was applied. Holograms were taken separately and the total span of the shell was recorded in separate holograms. Collimated illumination was utilized and the reconstruction pictures were taken far away from the location of the virtual image. In the second method, a modified single-hologram technique was utilized. Multiple points of observation in the plane of the hologram were employed to provide a way to minimize random errors. The first method proved to be adequate to measure displacements comprised between 10?4 to 10?5 in. The second method yielded results one order of magnitude better.  相似文献   

18.
论文根据堆本体内窄间隙同轴设备支承筒的结构特征、边界条件和窄间隙环腔内流体流速,将结构简化为一端固定一端自由的同轴圆柱壳,将圆柱壳内外的流体简化为无旋、无黏、不可压缩流体.同轴圆柱壳通过流体压力场实现耦合,其径向位移模态决定了窄间隙流体域的压力场,故采用级数形式的圆柱壳径向正交位移模态构建既满足一端固定一端自由边界条件...  相似文献   

19.
The paper describes how the Moiré reflective technique can be used to determine transverse-bending moments in a cylindrical shell. A cylindrical screen is used and the pattern of lines on it is reflected in the shell which acts as a lens and reduces the apparent pitch. When a photograph of the unloaded shell is considered, the lines on the negative are found to vary only slightly in width so that within the limits of movement of the ray reflected from the shell the pitch can be considered uniform. Loading the shell alters its radius and this alters the pitch of the lines as they appear on the photographic plate. It is shown that this change in line width does not affect the fringe pattern. Since the length of the reflected ray increases at distances away from the center of the photograph, a correction has to be applied to fringes at these points to obtain the correct change of slope. Photographs of the fringe pattern are obtained for various angular positions round the shell and, from these photographs, graphs of fringe against position round the shell are plotted. After correction, the slope of these graphs allows the bending moment at a point to be calculated. It is noted that transverse and radial deflections can influence the fringe pattern and this is allowed for. By taking photographs of the unloaded shell and measuring the widths of lines on the negative, the radius of the shell can be calculated and compared with spherometer readings. Knowing the bending moment at a point, the change in radius is calculated and the calculated final radius compared with that obtained from measurements on the separate photograph of the loaded shell. Finally, the deflections on the transverse center line are calculated from the fringe patterns and compared with deflection-gage readings.  相似文献   

20.
提出了一种分析含内埋矩形脱层正交各向异性圆柱壳稳定性问题的混合变量条形传递函数方法。首先基于Mindlin一阶剪切壳理论,通过定义圆柱壳的广义力变量和混合变量,建立了壳的改进混合变量能量泛函;然后,为了便于脱层壳的分区求解,通过引入条形单元,创建了基于混合变量条形传递函数解的含脱层和不合脱层两种超级壳单元;在此基础上,将含内埋矩形脱层的复合材料层合壳划分成两种超级壳单元的组合体,通过各超级壳单元相互之间连接结点处的位移连续和力平衡条件得到脱层壳的屈曲方程;最后由屈曲方程计算含内埋矩形脱层壳的屈曲载荷和屈曲模态。算例分析的结果验证了本方法的正确性,并给出了几种因素对屈曲载荷和屈曲模态的影响。  相似文献   

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