考虑接缝传荷的文克勒地基上矩形薄板的级数解

应用双重正弦级数展开的方法,推演得到了文克勒地基上计入两块矩形板间接缝传荷效应的级数解。假设接缝传递剪力与板间挠度差成正比、传递弯矩与板间转角差成正比,进而分析了单轮和单轴荷载作用在纵缝边缘中部时,接缝传荷效应对板边最大挠度和最大应力的影响规律;通过引入接缝传荷效应系数和接缝极限传荷的两个挠度比及两个应力比,建立了计入接缝传荷效应的板边最大挠度和最大应力的一般式,总结了不同板尺寸、荷载面积尺寸和类型及板材料泊松比对四个接缝影响系数和四个接缝极限传荷的挠度比及应力比的影响规律。结果表明:不同荷载面积下,受荷板接缝边缘最大挠度、最大应力均随弯矩或剪力传荷刚度系数的增大而减小,且应力的变化幅度相较挠度要小。影响系数fV^w(ξV)、fM^w(ξM)、fM^σ(ξM)与荷载圆相对半径(a/l)、相对板长(L/l)和相对板宽(B/l)无关,且单轮荷载与双轮荷载规律相同;而影响系数fV^σ(ξV)与荷载圆相对半径(a/l)有关,与相对板长(L/l)和相对板宽(B/l)无关;挠度比λV^w与荷载圆相对半径、板尺寸(L/l,B/l)及泊松比v无关,恒等于0.5,而λM^w、λV^σ、λM^σ均与荷载相对半径(a/l)、板尺寸(L/l,B/l)及泊松比v有关,且影响因素中荷载面积尺寸的影响最为显著。     

矩形板在面内荷载作用下的非线性屈曲分析

本文分析了具有不同面内边界条件的矩形板,面内受到常位移梯度偏心加载和常荷载偏心距加载的条件下的屈曲后性能和极限荷载.计算中同时考虑了板初曲和残余应力的影响,成功地将线性有线条理论推广应用于解决板的大挠度弹塑性稳定问题.这一方法与目前研究此类问题的其它方法相比较,在同等精度下计算工作量小得多.     

考虑地基水平摩阻的Winkler地基上板模型解析

在Winkler地基模型基础上,采用板与地基之间的水平摩阻应力正比于板与地基接触点间水平位移假设,推演了包含板弯曲和轴向拉压效应的非线性地基板微分方程;应用摄动法分析竖向集中力作用下,板与地基水平摩阻应力对板内力（弯曲力、轴向力和剪应力）、位移（挠度、水平位移）的影响规律,实证了板与地基水平摩阻应力对板剪应力的非线性影响可以忽略不计,从而得到了轴对称条件下计入地基水平摩阻的Winkler地基上薄板的线性微分方程．随后通过汉克尔变换得到了轴对称无限大板的解析解,以及包含四项复宗量贝塞尔函数的轴对称圆形板的解析解,给出了板内力、位移的计算式;最后,通过算例分析了板与地基间水平摩阻状况对板挠度、截面弯矩的影响规律．结果表明：地基板挠度与弯矩随着板与地基间水平摩阻的增大而减少;当地基板水平摩阻参数大于0.01时,地基水平摩阻力对板挠度和弯矩影响有可能超过2%,应予考虑;无限大板作用圆形均布荷载时,水平摩阻的存在最大可使板最大挠度（即荷载圆中心点处挠度）下降约50%,板最大截面弯矩（即荷载圆中心点处弯矩）下降约70%.     

弹性地基上无限大板的统一解

利用汉克尔变换法,推演得到了文克勒地基、双参数地基、弹性半空间体地基上无限大薄板,赖斯纳、汉盖、克罗姆等中厚板,在任意竖向荷载作用下的统一解;并给出了竖向轴对称荷载条件下的无限大板挠度、弯矩、剪力系数、地基反力系数的计算公式;最后,对圆形均布荷载作用下的不同地基和板模型的板挠度和弯矩进行了对比分析。结果表明:半空间体地基板与文克勒地基板的荷载圆中点的弯矩参数十分相近,但其荷载圆中点挠度系数较后者大1/3~1/2;中厚板理论对地基板挠度有更好地拟合和解析,但对板弯矩等内力的计算精度无改善。     

固支加筋方板的大挠度塑性动力响应

本文详细分析了爆炸载荷作用下固支回筋方板的大挠度塑性动力响应，给出了各种可能的运动模拟以及相应的差别条件，导出了最大残余变形的计算式，与文献［３］的试验结果比较表明，在多数情况下符合良好。     

初始缺陷对任意边界板极限承载力的影响分析

板钢结构承载力分析最终可化简为对一任意边界的矩形板在面内荷载作用下的极限承载力分析.从含初始弯曲的大挠度方程出发,以板厚度的折减量为摄动参数,将残余应力考虑成等效荷载,根据实用板与理想板的比较,得出板的厚度折减量和板的极限承载力方程.通过与非线性有限元方法和已有试验数据的验证分析,表明折减厚度法适用范围广、安全、精度高,可作为非线性有限元方法的补充,大大简化了结构极限承载力分析的复杂性.     

轴对称圆薄板大挠度微分方程的数值分析方法

根据轴对称问题的特点,利用级数展开和求极限法则,证明了轴对称大挠度圆薄板在圆心处应满足的边界条件,并以圆薄板轴对称大挠度弯曲变形微分方程为基础,建立了圆心处非奇异的轴对称大挠度圆板弯曲微分方程,从而可以方便地利用现有的常微分方程数值求解方法(如变步长龙格-库塔法)对实心圆板的轴对称问题进行数值求解,又不必像摄动法那样推导复杂的公式。在数值求解轴对称圆板大挠度弯曲变形微分方程时,将非线性微分方程的求解主要归结为迭代求解圆心处三个未知边界条件的问题,即圆心处的径向膜力、圆心处的挠度、圆心处挠度的二阶导数,并提出了相应的求解方法。实例中,对于圆薄板受均布横向荷载的问题,分析了周边固支边界条件下的非线性弯曲问题,给出了中心挠度参数大范围变化时的荷载和部分边界值变化曲线,并与经典摄动解进行了对比。对比结果可见,本文方法和摄动法的解非常接近,在量纲归一化中心挠度不超过4.0时,两种方法解的相对误差均小于5.0%。另外,本文还分析了与挠度有关的液体压力作用下和集中荷载作用下周边固支圆板的非线性弯曲问题。通过算例可见:本文方法可以灵活处理不同的荷载问题;对于不同的问题,计算过程相似,不必推导复杂的计算公式,计算精度容易控制。     

双钢板混凝土组合板抗爆性能分析

钢-混凝土-钢组合板是一种新型的组合结构,与传统钢筋混凝土板相比,具有抗剪强度高、延性大、耗能能力强等特点,目前已经被广泛应用于核反应堆安全壳、海洋平台及储油罐等结构。本文中,设计并制作了缩尺的普通钢筋混凝土板和钢-混凝土-钢组合板,开展了在接触爆炸荷载作用下的实验研究,通过损伤分析、跨中最大挠度对比研究不同板的抗爆性能。基于ANSYS/LS-DYNA非线性有限元程序,研究了钢-混凝土-钢组合板的损伤模式、跨中最大挠度等,并与实验结果进行了对比分析,验证了有限元分析模型的准确性和适用性。参数化分析了炸药量、混凝土强度和钢板厚度等参数对钢-混凝土-钢组合板抗爆性能的影响规律。利用多参数回归分析方法,提出钢-混凝土-钢组合板跨中挠度的预测公式。结果表明:提高混凝土强度可以降低结构的塑性损伤, 增加钢板厚度可以有效降低钢-混凝土-钢组合板的跨中最大挠度。相对于普通钢筋混凝土板,钢-混凝土-钢组合板保持了良好的整体性,且具有继续承载的能力。拟合公式能够较好地预测钢-混凝土-钢组合板跨中挠度与药量和钢板厚度的关系。     

不同拉压弹性模量椭圆板的非线性弯曲

把不同拉压弹性模量的椭圆板看成两种材料组成的层合板,采用弹性理论建立了在均布外载荷作用下的静力平衡方程,确定了中性面位置,求得了椭圆板中心挠度与均布荷载的关系;并把该方法计算结果与有限元方法计算结果进行比较,验证了方法可靠性。算例表明,当椭圆板材料拉压弹性模量相差较大时,挠度计算不宜采用相同弹性模量理论。     

双参数地基圆(环)形板的边界剪力及其力学响应

针对目前考量双参数地基上圆形或环形板边界剪力中存在的一些不足,应用Hankel变换法求得双参数地基的解析解,研究了任意环状线荷载作用下双参数地基的挠度、转角及地基反力间的关系。指出双参数地基在线荷载处的转角差与表示横向联系的地基参数之乘积等于线荷载集度;环内的分布荷载仅影响环内侧转角,而环外分布荷载也仅影响环外侧转角;进而又给出了适用于双参数地基圆形或环形板的内/外边界剪力的简明表达式。最后分别给出了双参数地基上自由边界圆形薄板中点承受集中力、圆形均布荷载作用时边界剪力对板中点挠度、弯矩的影响规律;双参数地基边界剪力对板挠度、弯矩有较明显影响,尤其是板的相对半径ρ_04或是荷载距板边界较近时这种影响更为明显。     

Fracture mechanics of laminated glass subjected to blast loading

A failure criterion based on energy balance approach is introduced for the laminated glass panel subjected to blast loading. Based on this failure criterion, a damage factor is developed to assess the failure of the laminated glass panel. If the damage factor is less than one, the plate is safe otherwise unsafe. Trigonometric function is employed to express the transverse deflection and the Airy’s stress function in von Karman’s large deflection equations of a thin plate. The nonlinear ordinary differential equation of motion obtained using the Galerkin method is solved using Runge–Kutta method. The predicted results indicate that the breakages of the laminated glass may be caused by the negative phase of the blast load if the positive phase blast load is not violent enough to cause failure. Also, the size of glass shards the laminated glass plies breaks in to is predicted using the surface energy based failure model.     

冲击波与破片对波纹杂交夹层板的联合毁伤数值研究

通过有限元软件LS-DYNA模拟了波纹杂交夹层板在冲击波与破片联合作用下的响应过程,研究了炸药当量、载荷类型和填充方式对波纹杂交夹层板变形与失效模式的影响,并与实体板、间隔板和波纹夹层板的抗联合毁伤性能进行了对比,讨论了波纹杂交夹层板的能量吸收特性。数值计算结果表明:与冲击波单独作用相比,破片群单独作用和冲击波与破片联合作用对结构造成的毁伤更为严重;当药量较小时,波纹夹层板和波纹杂交夹层板的抗联合毁伤性能优于实体板与间隔板,波纹杂交夹层板的抗联合毁伤性能从全填充、迎爆面填充到背爆面填充逐渐降低;当药量较大时,所有结构均产生破口失效;在能量耗散方面,冲击波单独作用时以波纹芯层吸能为主,破片群单独作用和冲击波与破片联合作用时以上面板吸能为主。     

Point-wise impulse (blast) response of a composite sandwich plate including core compressibility effects

This work analyzes the nonlinear impulse response of a composite sandwich plate exposed to a sudden point-wise transverse loading on the top face sheet. The nonlinearity arising from the core compressibility in the thickness direction is modeled and incorporated into the constitutive relations explicitly. As such, one can have a deep insight regarding the stress, strain and displacement profiles into the sandwich plate. The sandwich plate is assumed to be perfectly bonded at the face sheet/core interfaces. The equations of motion are formulated using Hamilton’s principle. The simply supported case is used to illustrate the procedure for solving the nonlinear equations. Numerical results are presented to demonstrate the response in terms of the transverse deformation and stresses in the composite sandwich plate. The effects of the variation of the geometrical parameters of the structure on the blast impulse response are also studied. Some conclusions are suggested regarding the associated optimal design of sandwich plates.     

横向爆炸载荷下开孔板的动应力集中因子

基于ANSYS 5.7/LS-DYNA程序,对3 m3 m0.25 m四边固支和简支、中心具有0.3 m0.3 m方孔的开孔板和无孔板对应点在两种下三角爆炸载荷作用下的应力响应进行了分析;由开孔板和无孔板边对应点的主应力时程曲线,对提出的能量密度时间分布函数的绝对值平方进行变上限积分,按其比值确定动应力集中因子,该方法简单易行。     

TNT空爆载荷下WELDOX 700E钢变形行为研究

以WELDOX 700E钢为研究对象，研究了8 mm钢在6 kg球形TNT空爆载荷、12 mm钢在10 kg球形TNT空爆载荷下的抗爆轰变形行为，结合ABAQUS模拟计算软件建立了WELDOX 700E钢抗爆轰变形模拟计算模型。结果表明:材料强度是影响WELDOX 700E钢抗爆轰变形行为的关键因素之一，高强度WELDOX 700E钢在球形TNT空爆载荷条件下呈现均匀的拱形变形。在6 kg球形TNT空爆载荷下，8 mm WELDOX 700E钢板中点的最大动态位移为144 mm，永久挠度为124 mm，回弹为21 mm；在10 kg球形TNT空爆载荷下，12 mm WELDOX 700E钢板中点的最大动态位移为166 mm，永久挠度为143 mm，回弹为23 mm。在不考虑实验工装整体偏移的条件下，球形TNT空爆载荷下钢的抗爆轰变形模拟计算结果可准确反映WELDOX 700E钢的抗爆轰变形行为。WELDOX 700E钢在抗爆轰形变过程中存在显著的厚度减薄现象并伴随一定的应变硬化行为，应变硬化行为主要为WELDOX 700E钢马氏体晶粒内部位错増殖的表现，8 mm和12 mm WELDOX 700E钢中心区域的位错密度较边部分别增加80.31%和151.76%。     

轻质金属泡沫夹芯曲板的抗爆炸冲击响应研究

夹芯结构具有高比强度、高比刚度和优异的吸能能力,已经被广泛应用于工程结构用来抵御高强度的爆炸冲击载荷。本文采用有限元数值模拟方法研究了爆炸载荷作用下四边固支夹芯曲板的动力响应。比较了同等质量下夹芯曲板、夹芯平板、实体曲板和实体平板四种结构的抗爆炸冲击性能,讨论了不同曲率和非对称因子对结构动力响应的影响,得到了使得夹芯曲板抗爆炸性能最佳的非对称因子。研究结果表明：夹芯曲板的抗爆炸冲击性能优于等质量的夹芯平板、实体曲板和实体平板结构,增大夹芯曲板的曲率能够提高结构的抗爆炸冲击性能。     

斜拉桥主梁模型承载性能试验研究

通过对斜拉桥主梁模型在不同工况及施加横向预应力方案的电测试验,得出了主梁的应力分布规律。试验结果表明,箱梁的撑杆和横向预应力的设计,对箱梁顶板的应力状态有很大影响。施加斜索力后,箱梁顶板的横向拉应力均小于1MPa,除横向预应力作用区域外,箱梁顶板的纵向应力为均匀分布的压应力,若在所有撑杆截面施加横向预应力,则撑杆只出现压应力。文中的试验数据可为优化结构、不同设计方案的选择提供理论根据。同时设计了对模型施加预应力的方法,解决了模型预应力的模拟问题。     

An analytical solution for underground structure-country rock dynamic interaction

In this paper according to the results of a great quantity of tests and numerical calculations, it is pointed out that the surrounding rock with thickness of 1/3 span has mechanical characteristics of a thick flexural member in underground rock cave subjected to transverse blast loading. However, it approaches the stress state of free field outside country rock and the equation of thick plate theory under the loading of free field pressure may be applied to the solution of this problem. Therefore, the underground structure-country rock dynamic interaction may be described by dynamic equations of flexural members of thin plate and thick plate, which express linear and country rock respectively. The interaction force between the liner and country rock is expressed as contacting pressure function q(x, l). By solving system of simultaneous equations, the analytical solution for the dynamic analysis of arch-straight liner including elastic half space interaction effect is given and the analytical expression of function q(x, t) is obtained. This analytic solution will contribute to the study of some substantive problems of underground structure-medium dynamic interaction theoretically. (Instutute of Engineering Mechanics, Academia Sinica)     

Blast Performance of Sandwich Composites with In-Plane Compressive Loading

An experimental investigation was conducted to evaluate the dynamic performance of E-glass Vinyl Ester composite face sheet / foam core sandwich panels when subjected to pre-compression and subsequent blast loading. The sandwich panels were subjected to 0 kN, 15 kN and 25 kN of in plane compression respectively, prior to transverse blast wave loading with peak incident pressure of 1 MPa and velocity of 3 Mach. The blast loading was generated using a shock tube facility. During the experiments, a high-speed photographic system utilizing three digital cameras was used to acquire the real-time 3-D deformation of the sandwich panels. The 3D Digital Image Correlation (DIC) technique was used to quantify the back face out-of-plane deflection and in-plane strain. The results showed that in-plane compressive loading facilitated buckling and failure in the front face sheet. This mechanism greatly reduced the blast resistance of sandwich composites.     

Suggestion of a new dimensionless number for dynamic plastic response of beams and plates

Summary A dimensionless number, termed response number in the present paper, is suggested for the dynamic plastic response of beams and plates made of rigid-perfectly plastic materials subjected to dynamic loading. It is obtained at dimensional reduction of the basic governing equations of beams and plates. The number is defined as the product of the Johnson's damage number and the square of the half of the slenderness ratio for a beam; the product of the damage number and the square of the half of the aspect ratio for a plate or membrane loaded dynamically. Response number can also be considered as the ratio of the inertia force at the impulsive loading to the plastic limit load of the structure. Three aspects are reflected in this dimensionless number: the inertia of the applied dynamic loading, the resistance ability of the material to the deformation caused by the loading and the geometrical influence of the structure on the dynamic response. For an impulsively loaded beam or plate, the final dimensionless deflection is solely dependent upon the response number. When the secondary effects of finite deflections, strain-rate sensitivity or transverse shear are taken into account, the response number is as useful as in the case of simple bending theory. Finally, the number is not only suitable to idealized dynamic loads but also applicable to dynamic loads of general shape. Received 17 October 1997; accepted for publication 19 March 1998