加劲钢板剪力墙弹性抗剪屈曲性能研究

系统地分析了三个主要参数(板高厚比λ、肋板刚度比η和柱刚度β)对钢板剪力墙弹性屈曲性能的影响;提出了钢板剪力墙的三种弹性屈曲形式(局部屈曲、整体屈曲和相关屈曲),指出肋板刚度比η=40时(相当于I s=3.7bt3)能保证十字加劲板发生小区格板的局部屈曲或整块板的相关屈曲;指出现行高层建筑钢结构规范用于纵横加劲板局部屈曲荷载的设计表达式仅适用于η≥40的条件,而在η<40范围内,其计算结果偏于不安全;研究了交叉加劲板的弹性屈曲荷载,并与非加劲板和十字加劲板的屈曲性能进行了比较;最终给出了柱刚度对弹性屈曲荷载的修正系数,提出了交叉加劲板弹性屈曲荷载的简化计算公式。     

具有初始应力加劲板的非线性动力学特性

针对工程结构中常用的加劲板,研究了其在初始应力作用下的非线性振动特性。将母板与加劲肋分开考虑,其中母板按薄板理论考虑,加劲肋按Euler-Bernoulli梁理论考虑,根据母板与加劲肋的应力与应变关系建立系统的应变能表达式,同时结合系统的动能表达式,并利用Lagrange方程建立系统的非线性动力微分方程。运用椭圆函数求得加劲板单模态的非线性频率,采用同伦分析方法求解加劲板的3∶1内共振。通过参数分析,重点讨论初始应力变化对系统非线性动力特性的影响,并得出初始应力的存在对加劲板非线性动力特性的影响规律。     

竖向槽钢加劲钢板剪力墙剪切屈曲

对设置多道竖向闭口加劲肋的钢板剪力墙的剪切屈曲进行了有限元弹性屈曲分析,得到了剪切应力随加劲肋抗弯和加劲肋抗扭刚度变化曲线,以加劲板临界应力等于小区格按简支计算的剪切屈曲应力为条件,得到了双面加劲肋的门槛刚度。刚度小于门槛刚度时给出了剪切屈曲临界应力与加劲肋刚度的关系;将双面加劲同单面加劲、交错单面加劲两种情况进行比较,得出了后两者的门槛刚度放大系数。与数值结果比较表明:公式具有良好精度且偏安全。     

带加劲肋十字型钢管节点支管轴压的承载力研究

针对带加劲肋十字型钢管节点采用有限元方法和足尺试验研究其承载力,比较两种方法的计算结果,探讨有限元中钢管节点屈曲的模拟方法,分析加劲肋贯穿对承载力的影响,最后将试验和计算结果与规范进行比较。研究表明:加带加劲肋十字型钢管节点支管轴压的最终破坏形态为环板的面外失稳;有限元中初始缺陷的最大幅值取主管管径的1/1000进行钢管节点屈曲分析是合理的;加劲肋贯穿主管的工艺可以一定程度上提高节点的刚度和承载力。     

初始缺陷对冷弯薄壁卷边槽钢梁局部相关屈曲的影响

本文根据含有初始几何缺陷的大挠度非线性Ｍａｒｇｕｅｒｒｅ方程，采用Ｇａｒｌｅｒｋｉｎ变分法，对受弯卷边槽钢板组的局部相关屈曲及初始几何缺陷对其局部相关屈曲的影响作了理论分析 。，并提出了考虑初始几何缺陷的临界屈曲计算公式。     

四边简支加劲板的几何非线性自由振动及内共振

研究了加劲板非线性振动的求解方法与振动特性。将加劲板分为母板与加劲肋两个部分考虑,其中母板视为大挠度板,加劲肋视为Euler梁。分别建立板与加劲肋的应变能与动能的表达式,并用张量的形式表示。将应变能与动能代入Lagrange方程,得到一系列关于面内与面外广义坐标的非线性振动微分方程组,多模态解可以通过增量迭代法求出,而单模态解可以用椭圆函数表示。最后,对一个四边简支且不可移动的加劲板前4阶模态进行分析,分别讨论了两个方向设置不同数量加劲肋的情况下非线性自振频率与振幅的关系,并分析了系统的内共振,得到了加劲板非线性振动一些特性,对工程设计有一定的参考意义。     

钢板剪力墙加劲肋刚度及弹性临界应力研究

我国现行加劲钢板剪力墙整体屈曲临界应力计算公式来自密肋加劲板,但实际工程中采用的钢板剪力墙多采用1条或2条横向加劲肋。对1600多个加劲钢板剪力墙模型进行了三维有限元弹性屈曲分析,深入研究了仅设置竖向加劲肋、竖向和1条横向加劲以及竖向和2条横向加劲肋钢板的加劲肋门槛刚度要求。并提出了加劲钢板剪力墙弹性剪切临界应力计算公式。与数值模拟结果的比较表明,新公式具有良好的精度,并且公式结果均在安全一侧,有望在工程中得到应用。     

梁柱端板连接节点的初始刚度计算

将节点分为受弯端板、受弯柱翼缘和受剪节点域三类组件,分别计算各组件的初始刚度并将其进行组装,提出了端板连接节点初始刚度的理论计算方法。该方法考虑了端板有加劲肋、无加劲肋两种构造形式,考虑了螺栓预拉力对节点刚度的影响,考虑了柱翼缘对节点域刚度的贡献,通过与试验和有限元结果对比表明该方法具有足够的精度,可用于节点刚性的判断。最后利用理论方法对按照现行规范设计的端板连接节点刚性进行了初步评价,并讨论了端板加劲肋的影响。     

U肋加劲板焊接残余应力的一种简化计算方法

基于焊接残余应力数值模拟方法, 分析了U 肋加劲板各组成板件的板宽、板厚对焊接残余应力分布的影响, 揭示了U 肋与母板残余应力合力的分配规律, 提出了针对不同构造尺寸的U 肋加劲板焊接残余应力分布简化计算方法。研究结果表明:各组成板件的板宽变化对焊接残余拉应力的分布影响较小, 但对焊接残余压应力的大小影响较大;U 肋与母板的板厚比对U 肋与母板残余应力的分配比例影响较大。U 肋加劲板受压承载力计算时, 焊接残余应力分布可以采用简化方法计算, 其结果与根据数值模拟得到的焊接残余应力分布计算的结果基本一致。     

竖向闭口加劲钢板剪力墙在非均匀压力下的弹性稳定性研究

对非均匀压应力作用下设置多道竖向闭口加劲肋的钢板剪力墙进行了有限元弹性屈曲分析,得到了屈曲临界应力随加劲肋加劲系数变化的曲线,以及各情况下的门槛刚度值。加劲肋门槛刚度随偏压系数增大而减小,随加劲肋数目增多而增大,随小区格宽高比增大而减小,随加劲肋扭弯比增大而减小。提出了竖向闭口加劲钢板剪力墙弹性屈曲加劲肋门槛刚度的近似计算公式,公式计算结果偏于安全。     

Numerical analysis of dynamic buckling of rectangular plates subjected to intermediate-velocity impact

This paper numerically investigates the dynamic buckling of thin imperfect rectangular plates subjected to intermediate-velocity impact loads. From numerical results obtained, a dynamic buckling and a dynamic yielding critical condition are defined, and the corresponding critical dynamic loads are estimated. Numerical model employed in the present study is validated by experimental data reported earlier. Results from parametric study indicate that initial imperfection and load duration have significant influence on the dynamic buckling of the plates. The smaller the initial imperfection and the load duration, the higher the dynamic buckling critical loads of the plates. Moreover, different hardening ratios of plate material also affect the elastic–plastic dynamic buckling properties of the plates. If the plate buckles plastically, the dynamic buckling load increases as the hardening ratio of plate material increases. Unlike thin plates under high-velocity impact that buckling always occur after load application, plates under intermediate-velocity impact analyzed in the present study all buckle during the loading phase.     

爆炸载荷作用下双向加筋方板的大挠度塑性动力响应

从分别列出加筋板面板以及加强筋的运动方程出发,分析了爆炸载荷作用下双向加筋固支方板的大挠度塑性动力响应。分析表明:取决于加强筋的相对刚度以及爆炸载荷峰值的大小,加筋板的运动将呈现3种不同的模式。该文限于讨论加筋板的总体变形模式,具体讨论了十字加筋以及双十字加筋固支方板在忽略弯矩影响下的薄膜解法。理论结果与已有的试验结果在多数情况下符合良好,表明该文提出的简化理论分析方法能对爆炸载荷下双向加筋方板的永久变形做出较为合理的预报。     

Thermal Postbuckling Analysis of Imperfect Reissner-Mindlin Plates on Softening Nonlinear Elastic Foundations

A thermal postbuckling analysis is presented for a simply supported, moderately thick rectangular plate subjected to uniform or nonuniform tent-like temperature loading and resting on a softening nonlinear elastic foundation. The initial geometrical imperfection of the plate is taken into account. The formulations are based on the Reissner-Mindlin plate theory considering the first-order shear-deformation effect, and including plate-foundation interaction and thermal effects. The analysis uses a deflection-type perturbation technique to determine the thermal buckling loads and postbuckling equilibrium paths. Numerical examples are presented that relate to the performances of perfect and imperfect, moderately thick plates resting on softening nonlinear elastic foundations. The effects played by foundation stiffness, transverse shear deformation, plate aspect ratio, thermal load ratio and initial geometrical imperfections are studied. Typical results are presented in dimensionless graphical form and exhibit interesting imperfection sensitivity.     

Optimum buckling design of composite stiffened panels using ant colony algorithm

Optimal design of laminated composite stiffened panels of symmetric and balanced layup with different number of T-shape stiffeners is investigated and presented. The stiffened panels are simply supported and subjected to uniform biaxial compressive load. In the optimization for the maximum buckling load without weight penalty, the panel skin and the stiffened laminate stacking sequence, thickness and the height of the stiffeners are chosen as design variables. The optimization is carried out by applying an ant colony algorithm (ACA) with the ply contiguous constraint taken into account. The finite strip method is employed in the buckling analysis of the stiffened panels. The results shows that the buckling load increases dramatically with the number of stiffeners at first, and then has only a small improvement after the number of stiffeners reaches a certain value. An optimal layup of the skin and stiffener laminate has also been obtained by using the ACA. The methods presented in this paper should be applicable to the design of stiffened composite panels in similar loading conditions.     

Buckling response of laminated composite stiffened plates subjected to partial in-plane edge loading

This article presents the buckling analysis of laminated composite stiffened plates subjected to partial in-plane edge loading. The finite element method is used to carry out the analysis. The eight-noded isoparametric degenerated shell element with C⁰ continuity and first-order shear deformation and a compatible three-noded curved beam element are used to model the plate skin and the stiffeners, respectively. The eigen value analysis is carried out to track the buckling load. The convergence study is performed for some specific problems and the results are compared with the available results in the literature. It is observed that the convergence of results is very fast for this finite element model. Effect of different parameters like orientation of fibers, number of layers, and loading types are considered in the present investigation. It is also observed that all these parameters have significant effect on the buckling response of the composite stiffened plate.     

Research on nonlinear torsional buckling and post-buckling of eccentrically stiffened functionally graded thin circular cylindrical shells

This paper is presented to solve the nonlinear buckling and post-buckling problem of functionally graded stiffened thin circular cylindrical shells only under torsion by the analytical approach. The shells are reinforced by rings and stringers attached to their inside and the material properties of shell and the stiffeners are assumed to be continuously graded in the thickness direction. Theoretical formulations based on the smeared stiffeners technique and the classical shell theory with the geometrical nonlinearity in von Karman sense are derived. Approximate three-term solution of deflection is chosen more correctly and the explicit expression to finding critical load and post-buckling torsional load–deflection curves are given. The effects of various parameters and the effectiveness of stiffeners on the stability of shell are shown.     

Buckling analysis of corrugated plates using a mesh-free Galerkin method based on the first-order shear deformation theory

This paper deals with elastic buckling analysis of stiffened and un-stiffened corrugated plates via a mesh-free Galerkin method based on the first-order shear deformation theory (FSDT). The corrugated plates are approximated by orthotropic plates of uniform thickness that have different elastic properties along the two perpendicular directions of the plates. The key to the approximation is that the equivalaent elastic properties of the orthotropic plates are derived by applying constant curvature conditions to the corrugated sheet. The stiffened corrugated plates are analyzed as stiffened orthotropic plates. The stiffeners are modelled as beams. The stiffness matrix of the stiffened corrugated plate is obtained by superimposing the strain energy of the equivalent orthotropic plate and the beams after implementing the displacement compatibility conditions between the plate and the beams. The mesh free characteristic of the proposed method guarantee that the stiffeners can be placed anywhere on the plate, and that remeshing is avoided when the stiffener positions change. A few selected examples are studied to demonstrate the accuracy and convergence of the proposed method. The results obtained for these examples, when possible, are compared with the ANSYS solutions or other available solutions in literature. Good agreement is evident for all cases. Some new results for both trapezoidally and sinusoidally corrugated plates are then reported.     

Stiffened cracked plates analysis by dual boundary element method

In this paper a boundary element formulation for analysis of shear deformable stiffened cracked plates is presented. By coupling boundary element formulation of shear deformable plate and two dimensional plane stress elasticity, dual boundary integral equations are presented. The interaction forces between stiffeners and the plate are treated as line distributed body forces along the attachment. Both concentric and eccentric stiffeners have been considered. Rectangular stiffened plate containing a single crack and double cracks subjected to uniform distributed moment on the crack surface and uniform shear load on the plate are analysed by the proposed method. Good agreement has been achieved compared with analytical solutions.