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1.
斜交板梁桥的有限单元算法   总被引:2,自引:0,他引:2  
借助斜坐标与直角坐标的关系,构造了斜交板梁单元的位移函数,由此提出了斜交板梁桥的实用有限单元算法。  相似文献   

2.
基于有限条带思想,引入结点扭率自由度,利用深梁单元的位移模式建立了一个4结点16自由度中厚板弯曲高阶单元,此单元是薄板单元BFS-16的推广形式,其特点是单元的横向位移、转角位移、剪应变位移模式直接构造,在边界上位移模式与深梁单元一致,方便与梁单元叠加,适应于带加劲肋的板弯曲问题分析,用于薄壁结构时可考虑翘曲。实例计算显示,此单元精度高,计算稳定,收敛快,无剪切闭锁现象,能较好地反映中厚板的边界效应。  相似文献   

3.
基于有限条带的厚/薄板矩形通用单元   总被引:1,自引:0,他引:1  
基于两广义位移梁理论,利用解析试函数来建立厚/薄梁单元的横向位移、转角位移、曲率、剪应变等位移模式,构造出厚/薄梁通用单元.应用有限条带,将厚/薄梁单元的位移模式应用于厚/薄板矩形弯曲单元,直接构造出单元的横向位移、转角、曲率、剪应变,导出了单元的刚度矩阵和结点等效力,编制了计算程序,进行了数值计算和比较,结果表明,所研究的单元不出现剪切闭锁且精度较好.  相似文献   

4.
龚克 《江苏力学》1996,(11):100-107
经典的梁板弯曲理论由于未考虑横向剪切变形的影响而只能适用于细长梁和薄板,传统的多广义位移的深梁理论和中厚板理论由于忽视了转角与挠度之间的内在关系而只能适用于短粗梁和中厚板。  相似文献   

5.
基于位移的有限梁单元中三次Hermite插值函数不能有效地描述变截面梁单元内部位移变化,只能通过加密网格增加单元数解决,会造成计算量增大。基于力的有限梁单元由于使用的力插值函数不受截面形状变化的影响,在处理变截面梁时有很大优势,可以得到精确的位移插值函数,利用较少的单元可以达到很高的精度,解决了基于位移的有限梁单元在处理变截面梁时的不足。本文得到了考虑剪切变形的位移插值函数和考虑转动惯量的一致质量矩阵。利用算例验证了本文理论的正确性和高效性。  相似文献   

6.
张延庆  龙驭球 《力学学报》1995,27(2):239-244
根据广义协调原理,首先利用Ferguson曲面构造出薄板弯曲单元,将中厚度板视为双向深梁,由Timoshenko理论拟合单元边界,利用Ferguson曲面的张量积性质,将薄板单元推广到中厚度板。数值结果表明此单元精度高,适应性强,且不出现剪切闭锁现象。  相似文献   

7.
本文从部分协调的三角形薄板弯曲单元出发,并假设横向剪切应变在单元内线性变化,提出了一种考虑横向剪切变形有具有15个自由度的三角平板弯曲单元。该单元应用于薄板和中等厚度板分析均有较高的精度,计算效率高,可用于工程中具有复杂形状的薄板和中等厚度板结构的分析。  相似文献   

8.
本文全面讨论了基于平面弹性--板弯曲模拟关系的薄板有限单元的理论和方法,由于直接对弯矩函数进行插值,c1连续性的要求得以自然避免,薄板单元可以直接在c0连续的层面上加以构造,无需借用Reissner-Mindlin的中厚板理论,由之引发的闭锁问题也得以避免,本文系统地阐明了平面弹性膜单元与薄板弯曲单元的对应关系,及由平面弹性膜单元的向薄板弯曲单元转换的一整套方法。为薄板单元的构造提供了一条新的有余的途径,文中给出了对应于平面弹性膜单元CST,LST,Q4,Q8的薄板单元,我们称之为MPS板单元,MPS板元以挠度和转角为自由度,便于实际应用,和其它板单元相比具有非常高的精度。  相似文献   

9.
曲线加筋Kirchhoff-Mindlin板自由振动分析   总被引:2,自引:2,他引:0  
相比传统加筋板,曲线加筋板能够更充分地发挥材料力学性能.在加筋板力学分析中,厚板通常采用Reissner-Mindlin理论,然而当板厚较薄时易出现剪切自锁,离散的Kirchhoff-Mindlin理论采用假设剪切应变场可避免该问题.针对曲线加筋Kirchhoff-Mindlin板自由振动分析,采用离散的Kirchhoff-Mindlin三角形单元和Timoshenko曲梁单元分别模拟板和加强筋,根据板的位移插值函数及筋板交界面的位移协调条件,建立基于板单元位移自由度的有限元方程.为了验证方法的有效性和准确性,采用直线加筋薄板、曲线加筋薄板和厚板3种模型进行算例研究,通过收敛性和精度分析来选择合理的有限元网格密度.直线加筋薄板前20阶固有频率均与文献结果吻合良好;曲线加筋板算例中,本文方法满足收敛条件的板单元数目为2469,Nastran模型板单元数目为6243;本文所得曲线加筋板固有频率与Nastran计算结果最大误差为3.4%.研究结果表明,本文方法无需筋板单元共节点,可使用较少的有限元网格数量,并能够保证计算精度;在离散Kirchhoff-Mindlin三角形板单元基础上构造Timoshenko梁单元可同时适用于曲线加筋薄板与厚板自由振动分析.  相似文献   

10.
本文从部分协调的三角形薄板弯曲单元出发,并假设横向剪切应变在单元内线性变化,提出了一种考虑横向剪切变形的具有15个自由度的三角平板弯曲单元。该单元应用于薄板和中等厚度板分析均有较高的精度,计算效率高,可用于工程中具有复杂形状的薄板和中等厚度板结构的分析。  相似文献   

11.
运用摄动理论首次将Reissner板理论分解为一系列Kirchhof板理论的叠加。这样,Reissner板问题的解答就可通过在具体边界条件下求解一系列Kirchhof板问题来获得。算例表明,本文方法简单,只需摄动两次就能接近Reissner板理论的精确解,适合在实际工程中推广  相似文献   

12.
板裂纹位置的确定   总被引:5,自引:0,他引:5  
本文研究了悬臂板的裂纹检测问题,提出了特征参数与加权特征参数法.所提利用故障结构的一阶特征对及无裂纹时的刚度阵与质量阵,确定结构裂纹位置的方法,既可用于简单的结构元件,也可用于复杂结构.算例与实验表明,所提方法可行.  相似文献   

13.
A thin plate has the form of the infinite strip ?∞<x<∞, 0≤yaand has the edge y=abuilt-in. The edge y=0 has its right half 0<x<∞ built-in while the left half ?∞<x<0 is free. The whole plate is now subjected to a uniform load p 0applied to its upper surface. What is the resulting deflection of the plate and what are the induced moment and shear resultants? We present a solution to this classical problem based on eigenfunction expansions. In the right and left halves of the strip, the deflection can be expanded as separate eigenfunction expansion series, but these are difficult to match across the line x=0 because of the singularity at (0,0) induced by the boundary conditions. We adopt the novel technique of expanding the field near the centre of the strip in its correct form as a series of Williams polar eigenfunctions, and then linking this expansion to the right and left eigenfunction expansions by using a special form of elastic reciprocity. These right and left reciprocity conditions give two infinite systems of linear equations satisfied by the polar expansion coefficients, and we prove that these equations are sufficient to determine these coefficients. Further applications of reciprocity give closed form expressions for the right and left eigenfunction expansion coefficients so that the whole solution is then determined. The method yields accurate results using small systems of linear equations. We present numerical results for the deflection of the plate and the induced moment and shear resultants.  相似文献   

14.
一种厚板薄板通用的新型广义协调元   总被引:2,自引:0,他引:2  
在适用于中厚板的八结点平板弯曲单元基础上,通过引入剪应变与位移的广义协调条件,建立起一种新型广义协调元,不仅保留了原单元适用于中厚板的特点,同时对薄板也给出了较精确的解,是一种厚板和薄板通用的新型广义协调元。  相似文献   

15.
本文用有限差分法对在轴对称荷载作用下的圆形折板壳屋盖进行静力分析,得到沿壳体径向内力。然后按GB110-89进行配筋及裂缝宽度、刚度计算。用BASIC语言,在SHARP PC-1500上实现。  相似文献   

16.
The dimensionless partial differential equations governing thedynamics of a thin flexible isotropic plate with an external load arederived and investigated. The period doubling bifurcations, as well asthe chaotic dynamics, are detected and analyzed. The algorithms leadingto the reduction of the original equations to those of a difference setof ordinary differential and algebraic equations are proposed, comparedto other known methods, and then applied to the problem.Among others, it is shown that, in spite of the system complexity, theFeigenbaum scenario exhibited by one-dimensional maps also governs theroute to chaos in the continuous system under consideration.  相似文献   

17.
本文利用二类变量广义变分原理推出了Mindlin板弯曲问题的Hamilton体系,利用辛几何方法对全状态向量进行分离变量,得到相应的横向本征问题,在求出其本征值后,按本征函数展开法导出了原问题的辛本征通解。给出了一个承受集中载荷的四边固支矩形薄板的算例,按本文求解体系得到的解与经典解吻合较好。本文直接从Mindlin板弯曲问题出发,在其Hamilton体系内使用辛几何方法给出了的一套新的求解体系,突破了传统解法的局限性,具有一般性及较高的理论推广价值。  相似文献   

18.
The stability of an unbounded plane elastic plate in gas moving on one side of the plate and at rest on the other is analyzed. The gases are inviscid and in general different. The plate is under tension and has flexural stiffness. It is shown that the system is always unstable to plane sinusoidal perturbations with wave vector parallel to the velocity. As limiting cases, a tangential discontinuity between the two gases and unilateral flow past a plate with constant pressure on the opposite side are considered. In these cases, the conditions of stability to plane perturbations are non-trivial and are investigated below.  相似文献   

19.
In this work, the finite element analysis of the elasto-plastic plate bending problems is carried out using transition rectangular plate elements. The shape functions of the transition plate elements are derived based on a practical rule. The transition plate elements are all quadrilateral and can be used to obtain efficient finite element models using minimum number of elements. The mesh convergence rates of the models including the transition elements are compared with the regular element models. To verify the developed elements, simple tests are demonstrated and various elasto-plastic problems are solved. Their results are compared with ANSYS results.The English text was polished by Keren Wang.  相似文献   

20.
The stability of an elastic plate in the form of a wide strip in a supersonic inviscid gas flow is investigated in the linear approximation. An expression for the dependence of the pressure on the plate deflection, asymptotically exact for wide plates, is used. Two qualitatively different instability types are obtained: flutter with respect to a single oscillatory mode due to negative aerodynamic damping and flutter of a related type due to the interaction of oscillatory modes. For each type the stability criterion and the frequency at which the oscillation amplitude grows most intensely are found.  相似文献   

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