侧向爆炸荷载下金属圆柱壳动力屈曲模态的实验研究

对金属圆柱壳在其中心部位经受75g柱状TNT炸药侧向爆炸冲击时的动力屈曲进行了实验研究,系统分析了3种壁厚的金属圆柱壳在不同爆炸距离下受侧向爆炸冲击的变形历程、最终变形模式和能量分配方式。得出了金属圆柱壳受侧向爆炸载荷时的4种典型屈曲模式及其相应的屈曲参数指标值,为金属柱壳结构爆炸破坏分级及结构抗爆设计提供了实验依据。     

充液金属薄壁圆柱壳轴向压缩屈曲性能实验研究

本文报导了充液金属薄壁圆壳轴向压缩屈曲性能的探索性实验研究，实验表明，由于壳内封闭液体存在，相比内空的金属薄壁圆柱壳屈曲性能表现出极大差异，如临界载荷有所提高，特别是“下临界载荷”显著提高，屈曲模态呈对称形式，后屈曲过程一直保持在较高载荷水平等。     

空爆荷载下爆源设置方式对圆柱壳动力响应的影响

基于动力有限元程序LS-DYNA及Euler-Lagrange耦合方法,分别以75g柱状和200g块状TNT炸药为爆源,对圆柱壳在爆炸载荷作用下的非线性动态响应过程进行三维数值模拟,描述了圆柱壳在不同爆源设置方式下的动力响应。数值模拟结果表明：壳壁破坏特征与药量Q、爆源设置方式密切相关,75g柱状TNT炸药轴线与圆柱壳轴线垂直设置时破坏作用大,而200g块状TNT炸药长边中心线与圆柱壳轴线平行设置时破坏作用则更强。研究结果为在役油气管道的抗爆能力分析和安全性评估提供了重要的参考依据。     

轴向冲击下复合材料圆柱壳的非对称动力屈曲

基于一阶剪切变形理论和非扁壳型几何方程，由Ｈａｍｉｌｔｏｎ原理导出包含初始几何缺陷的复合材料圆柱壳的非线性动力方程，Ｇａｌｅｒｋｉｎ方法得以位移形式表达的动力屈曲控制方程，通过有限差分方法求解，并由类似Ｂ－Ｒ准则方法判断动力屈曲是否发生；讨论了冲击速度，初始几何缺陷等因素对动力屈曲可能产生的影响。     

充液圆柱壳的波传播和功率流特性研究

以一无限长弹性充液圆柱壳为研究对象，分别用Ｆｌｕｇｇｅ壳体理论与Ｈｅｌｍｈｏｌｔｚ方程分析管壁结构波运动和管内声场，通过管壁内表面的运动协调条件，建立此耦合系统的运动微分方程。分析了耦合波的传播特点。重点讨论在自由传播波作用时，由壳体中各内力传播的功率流，从能量角度分析了各种波的传播特点。     

轴向冲击载荷下圆柱壳的塑性动力屈曲

对于轴向冲击载荷下圆柱壳的轴对称塑性动力屈曲问题。将临界应力和屈曲惯性项指数参数作为双特征参数求解．由相邻平衡准则导出失稳控制方程、边界条件和波阵面上的连续条件．由失稳瞬间的能量转换和守恒准则，导出波阵面上的一个屈曲变形约束方程．由此得出定量求解2个特征参数和动力屈曲模态的完备定解条件．关于屈曲应力和屈曲波数的理论计算结果与已有实验吻合良好．     

充满液体的薄壁圆柱壳轴向冲击屈曲实验研究

本文报导了一组曲型的充满水的金属薄壁圆柱试件轴向冲击屈过程的实验结果。     

圆柱壳冲击动力屈曲的研究

本文报导了圆柱壳在轴向冲南呼扭转冲击作用下动力屈曲的一些实验和分析结果，同时对充满液体的圆柱腔在轴向冲击作用下的屈曲过程和机理进行了探索性的研究，得到了些与内空的圆柱壳相比明显不同的特征。     

圆底扁球壳在任意集中脉冲荷载作用下的动力响应

本文利用经典小挠度弹性扁壳理论研究了圆底扁球壳在任意集中脉冲荷载作用下的动力响应问题。本方法具有收敛怏,计算工作量少的优点,计算结果在某些特殊情况下与有关文献的结果相一致。     

水下爆炸载荷作用下受损加肋圆柱壳的剩余屈曲强度计算

研究了在水下爆炸载荷作用下受损的加肋圆柱壳的屈曲．结合DYTRAN软件和NASTRAN软件计算了水下爆炸栽荷作用下受损的加肋圆柱壳的剩余屈曲强度，并且提出了一种结合上述两种软件计算加肋圆柱壳的剩余屈曲强度的方法．数值计算表明，预测结果与实验结果吻合较好．     

Nonlinear dynamic buckling of orthotropic cylindrical shells subjected to rapidly applied loads

Dynamic buckling of an orthotropic cylindrical shell which is subjected to rapidly applied compression is considered. A nonlinear differential equation of Donnell–Karman type is derived with the initial imperfection taken into account. An energy method is used to obtain the equation of motion which is then solved numerically by means of a Runge-Kutta method. These numerical results show that the critical load is increased over the corresponding static case. An analytical solution is also obtained for the problem of hydrostatic pressure.     

水下爆炸作用的单双层圆柱壳结构冲击损伤特性研究

针对圆柱壳结构受水下爆炸载荷冲击损伤问题用双渐近方法进行研究。通过大量工况分析发现,圆柱壳结构损伤模式按产生原因可分为直接冲击损伤引起局部结构强度破坏、局部构件横向冲击失稳、壳体环向冲击失稳及鞭状运动引起壳体纵向总体失稳4种,爆距较近时气泡脉动载荷占主要成分,较远时冲击波占主要成分。     

新型矩形蜂窝夹芯夹层加筋圆柱壳抗水下爆炸冲击载荷分析

提出了一种新型矩形蜂窝夹芯夹层加筋圆柱壳结构形式。分析了其在水下爆炸冲击载荷下的动力响应特征及     

Nonlinear dynamic buckling of functionally graded cylindrical shells subjected to time-dependent axial load

This paper is presented to solve the nonlinear dynamic buckling problem of a new type of composite cylindrical shells, made of ceram/metal functionally graded materials. The material properties vary smoothly through the shell thickness according to a power law distribution of the volume fraction of the constituent materials. The dynamic axial load is set in a linear increase form with regard to time. By taking the temperature-dependent material properties into account, the effect of environmental temperature rise is included. The nonlinear dynamic equilibrium equation of the shell was obtained by applying an energy method, and was then solved using the four-order Runge–Kutta method. The critical condition was eventually determined using B-R dynamic buckling criterion. Numerical results show the dynamic buckling load is higher than its static counterpart. Meanwhile, various effects of the inhomogeneous parameter, loading speed, dimension parameter, environmental temperature rise and initial geometrical imperfection on nonlinear dynamic buckling are discussed.     

Stochastic post buckling analysis of laminated composite cylindrical shell panel subjected to hygrothermomechanical loading

In this paper, the effect of random system properties on the post buckling load of geometrically nonlinear laminated composite cylindrical shell panel subjected to hygrothermomechanical loading is investigated. System parameters are assumed as independent random variables. The higher order shear deformation theory and von-Karman nonlinear kinematics are used for basic formulation. The elastic and hygrothermal properties of the composite material are considered to be dependent on temperature and moisture concentration using micromechanical approach. A direct iterative based C⁰ nonlinear finite element method in conjunction with first-order perturbation technique proposed by present author for the plate is extended for shell panel subjected to hygrothermomechanical loading to compute the second-order statistics (mean and variances) of laminated composite cylindrical shell panel. The effect of random system properties, plate geometry, stacking sequences, support conditions, fiber volume fractions and temperature and moisture distributions on hygrothermomechanical post-buckling load of the laminated cylindrical shell panel are presented. The performance of outlined stochastic approach has been validated by comparing the present results with those available in the literature and independent Monte Carlo simulation.     

钢质圆柱壳在侧向局部冲击荷载下的变形及失效破坏

基于动力有限元程序LS-DYNA及随动塑性Cowper-Symonds模型,对两端固支钢质薄壁圆柱壳经受半球头弹体侧向局部冲击的非线性动力响应问题进行数值模拟,获得了不同冲击条件下圆柱壳的变形及破坏模态,并研究了弹体在不同周向冲击倾角时壳壁产生穿透性破裂的最小速度（临界破裂速度）。研究表明,圆柱壳破坏模式与弹体冲击倾角θ0、冲击速度V等因素密切相关,将发生局部凹陷、碟形变形及穿透现象,且临界破裂速度随冲击倾角的增大而增大。研究结果可应用于圆柱壳在侧向局部冲击作用下的毁伤预测,从而为圆柱壳结构的安全防护设计提供理论依据。     

Nonlinear behavior and buckling of cylindrical shells subjected to localized external pressure

Buckling loads and postbuckling behavior of cylindrical shells subjected to localized external pressure are considered. The modified extended Kantorovich method with path-tracing technique is applied to determine the buckling loads of the cylindrical shells. It is found that the load is dependent nonmonotonically on geometrical parameters of the area subjected to external pressure. Respective postbuckling shapes show correlation with the shapes corresponding to secondary bifurcation paths for the cases of a cylindrical shell under uniform external pressure and a cylindrical shell under uniform axial load.     

Non-linear buckling and postbuckling of shear deformable anisotropic laminated cylindrical shell subjected to varying external pressure loads

Non-linear buckling and postbuckling of a moderately thick anisotropic laminated cylindrical shell of finite length subjected to lateral pressure, hydrostatic pressure and external liquid pressure has been presented in the paper. The material of each layer of the shell is assumed to be linearly elastic, anisotropic and fiber-reinforced. The governing equations are based on a higher order shear deformation shell theory with von Kármán–Donnell-type of kinematic non-linearity and including the extension/twist, extension/flexural and flexural/twist couplings. The non-linear prebuckling deformations and initial geometric imperfections of the shell are both taken into account. A singular perturbation technique is employed to determine the buckling pressure and postbuckling equilibrium paths. The numerical illustrations concern the postbuckling response of perfect and imperfect, moderately thick, anisotropic laminated cylindrical shells with different values of shell parameters and stacking sequence. The results confirm that there exists a circumferential stress along with an associate shear stress when the shell is subjected to external pressure.     

复合材料圆柱壳的轴压屈曲失效试验

为了研究高径比大于1的复合材料圆柱壳的轴压屈曲性能及其失效模式,对2组单向纤维圆柱壳和3组外侧环裹环向纤维圆柱壳进行了轴压试验,观察了试件的受力过程和破坏形态,获得了荷载-位移曲线和荷载-应变曲线,利用有限元模型分析了单向纤维圆柱壳两种屈曲形式的破坏机制,对比分析了两种铺层试件的轴压性能。结果表明:单向纤维复合材料圆柱壳出现先纵向劈裂后板壳屈曲和先柱壳屈曲后纵向劈裂的两种破坏模式;外侧环向纤维可改善圆柱壳的轴压性能,屈曲发展有一定的阶段性并表现出延性特征,破坏形式和承载力均较为稳定。     

Twin-characteristic-parameters analysis for elastic dynamic buckling of thin cylindrical shells under axial step loading

The relations of the critical stress and transverse inertia effect to the loading duration are investigated for the dynamic buckling of thin cylindrical shells under axial step loading. The critical stress and the inertial exponent are treated as the two characteristic parameters. The criterion of energy conservation is used to derive the supplementary restraint condition for buckling deformations at compression wave front. By use of the Galerkin method, an algebraic eigenvalue problem for the two characteristic parameters is derived from the governing equations and boundary conditions. The solution of the eigenvalue problem, which satisfies the supplementary restraint condition, gives the values of the critical stress and the inertial exponent for the dynamic buckling. The relation of critical stress to loading duration, predicted by the theoretical analysis, is in reasonable agreement with the experimental results.