• On the basis of classical lamination theory and large deflection hypotheses of plate, the equilibrium and compatibility equations of simply supported composite laminated plates were obtained.

    基于经典理论板的挠度基本假设得到四边的非线性运动方程及变形协调方程;

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  • The solutions of a large deflection problem of thin orthotropic circular plates with variable thickness under uniform pressure and under concentrated load are obtained in this paper.

    本文给出了正交异性厚度薄板均布载荷集中载荷作用挠度问题

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  • This phenomenon, paired with the heating of upper components can cause tube dings due to the deflection of the plates.

    现象伴随上部组件发热产生,并板材偏斜而导致管路弯折。

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  • The solution of large deflection problem of thin orthotropic circular plates with variable thickness under uniform pressure under simply supported boundary condition is obtained in this paper.

    本文给出正交各向异性厚度周边薄板均布载荷挠度问题

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  • The influence curve which shows the effect of the load and the damping medium on movement time and residual deflection of central point for circular plates was traced in this paper.

    文中画出了荷载阻尼介质运动时间中心点残余挠度影响曲线

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  • The result is a measurable change in the capacitance between the two plates that is proportional to the Angle of deflection.

    结果两个板块之间电容产生可测量改变这种改变与偏转角成比例的。

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  • According to theoretic analysis, computing the bending deflection of every roller is enabled to ignore the effect of the web and only allow to the rectangular section made up of flange plates.

    理论分析认为求解可调挠度时,可以不考虑腹板影响按翼缘组成的“矩形断面进行

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  • The large deflection problems of the symmetrically laminated cross-ply circular plates of fiber reinforced composites are investigated in this paper by using Galerkins procedure.

    本文探讨了纤维增强复合材料正交对称铺设层合挠度弯曲问题

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  • To begin with, in this paper, the displacement governing equations and the boundary conditions of nousymmetrical large deflection problem of circular thin plates are derived.

    本文首先导出圆薄板非轴对称变形问题位移基本方程边界条件

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  • Finally, the referencing formulas to calculate the rigidity and deflection of beams strengthen by gluing steel plates are proposed, and the calculating results cohere to the experimental results well.

    最后加固的刚度挠度计算提出参考公式试验结果吻合

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  • Again USES the model, through transformation composite beam highly and various steel plates parameter comparative analysis beam and support capacity, stress, deflection change and so on.

    再利用模型通过变换组合梁高度钢板的厚度等参数比较分析承载能力应力挠度变化等。

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  • Navier's solution of plates is an analytical expression on the deflection, which was derived from a boundary condition of simply supported rectangular plates at four sides.

    纳维叶矩形在四边边界条件下导出挠度解析表达式

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  • A new approach to the solution of large deflection bending problem of thin plates is presented by using boundary element method.

    本文提出一个边界求解薄板挠度弯曲问题途径

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  • Based on the tiny deflection theory of the elastic thin plates, the differential equations of the cellular voided plates are given.

    弹性薄板挠度理论为基础推导蜂窝式空心板微分方程。

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  • This paper presents a new solution of the large deflection dynamic response of stiffened plates under lateral impact loading.

    用半解析方法分析横向冲击载荷非线性响应

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  • Solving the thin plates on Winkler's foundation by the nonsingular boundary element method and the layerwise summation method, the deflection of the given point of the plate can be obtained.

    本文以无奇点边界分析地基,而用分层总和法计算地基沉降,并将两者联系起来,即利用边界元法下的地基反力作为分层总和法的外力,从而求出地基的沉降。

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  • The computation results show the cantilever plates which fiber is perpendicular to the clamped boundary has the minimum deflection. The effect of anisotropy on the deflections of the plate isd...

    分别选取强各异性材料、弱各向异性材料进行计算分析结果表明纤维方向垂直于悬臂固定层合悬臂板刚度挠度最小

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  • In nonlinear analysis, FGM plates and shells behaviors, which include large deflection bending, large deflection vibration, post-bucking, are discussed using Galerkin variational method.

    线性分析中,解析方法分析FGM、圆柱双曲率扁弯曲振动与屈曲等力学行为

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  • The deflection is assumed to be functions of complex variables, and then the moments and shearing forces of the plates can be obtained.

    首先假设挠度函数式,进而可以内力

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  • The deflection is assumed to be functions of complex variables, and then the moments and shearing forces of the plates can be obtained.

    首先假设挠度函数式,进而可以内力

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