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复合载荷作用下具有光滑中心波纹膜片的非线性分析 总被引:2,自引:0,他引:2
采用轴对称旋转壳体的简化Reissner方程,研究了在复合载荷作用下具有光滑中心波纹膜片的非线性弯曲问题。应用积分方程方法,可以获得膜片的特征关系(载荷-中心挠度关系)。文末给出了实例计算的数值结果。 相似文献
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均布载荷作用下带边缘大波纹膜片的非线性弯曲 总被引:6,自引:0,他引:6
采用轴对称旋转壳体的简化Reissner方程,研究了在均布载荷作用下具有硬中心的带边缘大波纹膜片的非线性弯曲问题.应用积分方程方法,获得了具有夹紧固定和滑动固定两种外边界的膜片的特征关系,即荷载-中心挠度曲线.作为算例,给出了夹紧固定膜片中的应力分布. 相似文献
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采用轴对称旋转壳体的简化Reissner方程,研究了在均布载荷作用下具有光滑中心波纹膜片的非线性弯曲问题。应用格林函数方法,波纹膜片的非线性边值问题化为了非线性积分方程的求解。为了求解积分方程并防止发散,一个插值参数被引入到迭代格式中。计算表明,当载荷很小时,任何插值参数值均能保证迭代的收敛性,取插值参数值接近或等于1获得较快的收敛速度,而当载荷较大时,插值参数值不能取得过大。绘出了波纹膜片的特征曲线,得到的特征曲线可供设计参考。可以断言,当载荷不大时,特征曲线是近似线性的,随着载荷的增大,特征曲线开始向上弯曲,明显偏离线性。本文中提出的解决方法适应于任意轴向截面的波纹壳体。 相似文献
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本文采用逐步加载法将圆板弯曲的非线性微分方程组线性化,再用变分方法求解线性化方程.文中推得各次加载时的载荷与挠度,应力与挠度关系的递推公式.圆形薄板在轴对称弯曲情况下的非线性问题可用卡门方程表示 相似文献
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1.几何非线性问题的基本方程在本世纪初,Reissner H.和Meissner E.利用在线性薄壳理论中存在的静力-几何比拟关系,将线弹性薄壳轴对称问题,归结为以应力函数和转角为未知量的两个常微分方程。以后,人们利用这两个方程的相似性,引入复未知函数,把一些典型壳体的方程简化为一个二阶变系数常微分方程,为这些问题的求解带来极大的便利。本文将这一方法推广到薄壳大位移问题,导出用复未知函数表示的常子午线曲率壳体轴对称变形的非线性微分方程。从这个一般方程可以直接得到关于柱壳,锥壳,圆球壳,环壳和圆板几何非线性问 相似文献
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?????? ?????? ?????? 《力学与实践》1996,18(4):24-25
本文采用常微分方程两点边值问题的打靶法,建立了圆薄板轴对称大挠度弯曲vonKármán位移型方程的自动求解过程.作为例子,分析了圆薄板在均布横向截荷作用下的非线性弯曲问题,给出了载荷参数大范围变化的解曲线 相似文献
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波纹壳是传感器弹性元件的一类重要形式,也是精密仪器仪表弹性元件中的一类重要形式。由于波纹壳形状复杂、参数众多、厚度薄,对其进行非线性分析非常重要同时也是十分困难的。本文考虑一种在传感器弹性元件中有重要应用价值的正弦波纹浅球壳体,将这种壳体视为结构上的圆柱正交异性扁球壳,根据Andryewa的思想,分别得到了正弦波纹壳径向、环向在拉伸、弯曲下的等价的四个各向异性参数;建立了正弦波纹扁球壳的非线性强迫振动微分方程;得到了正弦波纹扁球壳非线性强迫振动的共振周期解及幅频特性曲线。 相似文献
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By using the fundamental equations of axisymmetric shallow shells of revolution, the nonlinear bending of a shallow corrugated shell with taper under arbitrary load has been investigated. The nonlinear boundary value problem of the corrugated shell was reduced to the nonlinear integral equations by using the method of Green's function. To solve the integral equations, expansion method was used to obtain Green's function. Then the integral equations were reduced to the form with degenerate core by expanding Green's function as series of characteristic function. Therefore, the integral equations become nonlinear algebraic equations. Newton' s iterative method was utilized to solve the nonlinear algebraic equations. To guarantee the convergence of the iterative method, deflection at center was taken as control parameter. Corresponding loads were obtained by increasing deflection one by one. As a numerical example,elastic characteristic of shallow corrugated shells with spherical taper was studied.Calculation results show that characteristic of corrugated shells changes remarkably. The snapping instability which is analogous to shallow spherical shells occurs with increasing load if the taper is relatively large. The solution is close to the experimental results. 相似文献
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Yong-Gang Wang Xiao-Meng Li Dan Li Xin-Zhi Wang 《Archive of Applied Mechanics (Ingenieur Archiv)》2011,81(12):1925-1933
An integrated mathematic model and an efficient algorithm on the dynamical behavior of homogeneous viscoelastic corrugated
circular plates with shallow sinusoidal corrugations are suggested. Based on the nonlinear bending theory of thin shallow
shells, a set of integro-partial differential equations governing the motion of the plates is established from extended Hamilton’s
principle. The material behavior is given in terms of the Boltzmann superposition principle. The variational method is applied
following an assumed spatial mode to simplify the governing equations to a nonlinear integro-differential variation of the
Duffing equation in the temporal domain, which is further reduced to an autonomic system with four coupled first-order ordinary
differential equation by introducing an auxiliary variable. These measurements make the numerical simulation performs easily.
The classical tools of nonlinear dynamics, such as Poincaré map, phase portrait, Lyapunov exponent, and bifurcation diagrams,
are illustrated. The influences of geometric and physical parameters of the plate on its dynamic characteristics are examined.
The present mathematic model can easily be used to the similar problems related to other dynamical system for viscoelastic
thin plates and shallow shells. 相似文献
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IntroductionCorrugateddiaphragmisatypeofelasticthinshells .Itsdesignisverycomplicatedbecauseoftoomanyparametersthatinfluenceeachother.Inanumberofinstrumentsmeasuringdisplacements,corrugateddiaphragmissubjectedtoelasticdisplacementthatisatleastthesameorderasitsthickness,sothatitisnecessarytousegeometricalnonlineartheoryofthinshellstoanalyze.Sofarasweknow ,inmostcases,investigatorsdiscussedonlytheproblemofcorrugateddiaphragmwithuniformanddensecorrugationsundertheactionofaunique(uniformlyorconcen… 相似文献
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IntroductionTheplatesandtheshellswithvariablethicknessarewidelyusedinengineering .Theproblemaboutstaticshasbeenstudiedbymanyscholars;therearemanyRefs .[1 -4 ]inthisfield .Papersaboutnonlineardynamicsaremuchless[5 ,6 ].Inthispaper,selectingthemaximumamplitudeinthecenterofshallowconicalshellswithvariablethicknessasperturbationparameter,thenonlinearnaturalfrequencyofshallowconicalshellswithvariablethicknessisobtainedbymethodgiveninRef.[7] .Thenonlinearnaturalfrequencyisnotonlyconnectedwiththeva… 相似文献
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The governing equilibrium equations for strain gradient elastic thin shallow shells are derived, considering nonlinear strains and linear constitutive strain gradient elastic relations. Adopting Kirchhoff’s theory of thin shallow structures, the equilibrium equations, along with the boundary conditions, are formulated through a variational procedure. It turns out that new terms are introduced, indicating the importance of the cross-section area in bending of thin plates. Those terms are missing from the existing strain gradient shallow thin shell theories. Those terms highly increase the stiffness of the structures. When the curvature of the shallow shell becomes zero, the governing equilibrium for the plates is derived. 相似文献