圆柱壳开孔的应力分析

本文研究圆柱壳开孔附近的应力分析问题。由于开孔问题的边界形状较为复杂,使用圆柱壳的 Morley 方程进行求解较为困难。本文在进行误差分析的基础上提出修正 Mo-rley 方程,并给出适合于开孔问题边界的一般解。以圆柱壳受轴向拉伸和内压为例分析了开孔附近的应力分布。给出了开孔率为 1/2以下的开孔解,并对 Donnell 方程解的适用范围给予了新的评价。     

带有椭圆孔的各向异性无限板应力集中问题的简便解法

应用各向异性无限域椭圆孔问题的复应力函数基本解,给出了椭圆孔在任意外载作用下以积分形式表示的复应力函数解;并分别通过对椭圆孔周边均匀受载,无限远处均匀受载和承载螺栓孔这三个特例的分析结果,证实了本文解的正确性,一般性和实用性.     

无限大板开孔弹性波的散射及动应力集中

采用弹性平板理论及复变函数理论，对含孔无限大平板弹性波的散射及动应力集中问题进行了分析研究，建立了求解平板开孔动应力集中问题的复变函数方法。若同时采用映射变换，就为求解平板开任意形状孔的动应力集中问题提供了一种规范而有效的方法。为说明问题，本文给出了平板开圆孔及椭圆孔动应力集中因子的数值结果。     

含孔平板弹性波散射问题的复变函数方法

本文采用平板弯曲波动理论及复变函数方法，对平板开孔弹性波的散射及动应力集中问题进行了分析研究，得到了传播急剧记波时此种平板弯曲波动问题的分析解。若同时采用保角射技术，就为主解平板任意形状开孔弹性波的散射及动应力集中问题提供了一种统一规范的方法。作为算例，本文给出了平板开圆孔和椭圆孔附近的动应力集中系数的数值结果，并对其进行了讨论。     

开孔薄板的变分原理及屈曲和过屈曲分析的有限元方法

本文以开孔薄板大挠度问题的一般理论为基础,建立了以挠度 w 和应力函数F为未知量的变分原理,并由此建立了用于分析开孔薄板屈曲和过屈曲问题的有限单元法可以看到由于区域的多连通性,单元性质是较为复杂的。     

开孔粘弹性薄板的非线性数学模型

应力函数的多值性和位移单值性要求，是开孔薄板大挠度问题中必须注意的两个方面。本文利用线粘性力学中的Ｂｏｌｔｚｍａｎｎ蠕变律，把开孔弹性薄板大挠度问题的一般数学理论推广到开孔弹性薄板。在考察应力函数的多值性和位移单值性条件的基础上，提出了开孔粘弹性薄板的控制方程和初、边值条件，系统地建立了开也粘弹性薄板非线性分析的三类初一边值问题。     

开孔圆板的计算

开孔圆板,在料仓、泵房等结构中经常遇到。本文用选择开孔圆板孔洞中心为新极点,引入新坐标γ,θ作为非开孔圆板原坐标R,的参考系统的方法,解决了任意边界条件及荷载的开孔圆板的弯曲问题。利用本文方法及公式,不难编制出形变及应力的计算图表,供实际设计时应用。     

各向异性弹性体中矩形孔边缘应力分布

推导了各向异性平面弹性体中矩形孔洞边缘的应力分布公式并给出了数值计算结果。工程中会遇到矩形孔洞的问题，而矩形孔导致的应力集中增加了工程问题的复杂性。目前尚没有简单实用的公式计算矩形孔在各向异性体中应力的分布。本文采用复变函数保角变换的方法推导了矩形孔边缘的应力公式。在利用本文给出的方法，可以计算矩形孔在不同性质的各向异性材料中，承受任意的双轴荷载下孔边缘的应力分布情况。     

关于泡沫塑料各向异性模型的修正

本文研究了开孔泡沫塑料的力学各向异性问题。在已有模型的基础上，结合扫描电镜的分析结果提出了对Ｋａｎａｋｋａｎａｔ模型和Ｈｕｂｅｒ－Ｇｉｂｓｏｎ模型的修正。这种修正反映了开孔泡沫塑料支柱的横向尺寸比对泡沫塑料各向异性性质的影响     

开孔薄板的弯曲问题

本文利用边界型最小二乘配点法,取极座标下的双调和方程的特解序列作为试函数,对开大孔的薄板弯曲问题进行了计算研究。计算中应用了复变函数保角变换的技术,得到了具有正多边形孔的圆板弯曲问题的近似解。这种方法可推广至其它形状的孔与其它形状的外边界。此外,在计算过程中提出了试函数逐项加权的方法,在一定程度上改善了矩阵病态的情况。     

Perturbation analyses for the postbuckling of simply supported rectangular plates under uniaxial compression

In this paper, applving perturbation method to von Kármán nonlinear large deflection equations of plates by taking deflection as perturbation parameter, the posibuckling behavior of simply supported rectangular plates under uniaxial compresion is investigated. Two types of in-plane boundary conditions are now considered and the effects of initial imperfections are also studied. It is found that the theoretical results are in good agreement with experiments. The method suggested in this paper which has not been found in previous papers is rather simple and easy for the postbuckling analysis of rectangular plates.     

Ultimate strength of postbuckling for simply supported rectangular composite thin plates under compression

1.IntroductionAsiswellthnown,thepostbucklingmetalplatescanbesuccessivelysubjectedtotheload.Forsomemetalplates,theultimatestrengthcanreachthirtytimesofthebucklingstressll].Inordertostudythebearingcapacityofthecompositeplatesthroughtestsandtheoreticalanalysis,f'ttiluretestsofthe283specimensofGFRPthinrectangularplatesundercompres.sionarecarriedout.ItisprovedthattheGFRPplatesinpostbucklingstillhavehigherbearingcapacity,forthetestedspecimensshowedultimatestrengthwhichisfourtotwenty-livetiniesth…     

Elasto-plastic analysis for the buckling and postbuckling of rectangular plates under uniaxial compression

Full-range analysis for the buckling and postbuckling of rectangular plates under in-plane compression has been made by perturbation technique which takes deflection as itsperturbation parameter.In this paper the effects of initial geometric imperfection on the postbuckling behaviorof plates have been discussed.It is seen that the effect of initial imperfection on the inelasticpostbuckling of plates is sensitive.By comparison,it is found that the theoretical results ofthis paper are in good agreement with experiments.     

Buckling test and optimum design of fiber reinforced composite plates under compression

In this paper, the conclusion that the experimental results coincide with theoretical analysis has been got through buckling test of 283 composite rectangular plates. It is confirmed that the critical loads of composite plates calculated by buckling theoretical formula of anisotropic plate are reliable. The selections of optimal content of matrix and optimal off-axis which make fiber reinforced composite plates reach biggest critical loads are also discussed in this paper. The result of analysis may be used in the design for the products.     

无单元法分析弹性地基板

弹性地基板的计算是学和工程师们十分关切的问题,本提出了分析Ｗｉｎｓｌｅｒ地基、双参数地基和半空间弹性地基板弯曲问题的无单元法,推导了无单元法的插值函数,从变分原理出发导出弹性地基板的刚度矩阵,给出计算实例,与其它的方法的结果进行比较,数值结果表明无单元法具有一系列优点。     

Dynamical bending of rigid-plastic annular plates

Dynamical bending of circular rigid-plastic annular plates, fixed along the exterior boundary and free on the interior boundary, when subjected to instantaneously applied transverse uniformly distributed blast-type load[1], is investigated in this paper.It is shown that annular plates are preferable to plates without holes, since their load capacity increases while residual deflections decrease. A so-called boundary parameter is introduced to estimate the effect of boundary conditions on the radial bending moment.A procedure for determining the residual deflections at every point of a plate is developed for use on an electronic computer. Numerical examples are given. In the end of the paper, the particularities of solution of our problem for annular plates, corresponding to the setting of Wang[2], Wang and Hopkins[3] for plates without holes are discussed.     

静载荷作用下柔韧圆板的大幅度振动

本文首先给出了均布载荷作用下柔韧圆板的大幅度振动方程，按文中给出的时间模态假设导了该问题的非线性耦合的代数和微分特征方程组，利用修正迭代法求出了该方程组的近似解析解，得到了柔韧圆振动的幅频－载荷特征关系，讨论了静载荷对其振动性态的影响。     

复变形式的各向异性板弯曲问题的基本解

提出了求解各向异性板弯曲问题基本解的新方法。得到的基本解简捷明了，相应的法向弯矩和相当剪力的表达式易求，故便于应用在一般边界条件的各向异性板弯曲问题的边界积分方程。     

圆板在物体撞击下的非线性动力响应

本文在Von Kármán大位移的意义上,利用虚位移原理伽辽金方法建立了圆板在物体撞击下的非线性动力响应的控制微分方程,在研究响应问题时,考虑了冲击载荷与圆板位移响应之间的耦合影响,文中使用时间增量法和奇异摄动理论求解问题的控制方程,获得了固支圆板非线性动力响应的近似解,并且求解了具体算例,绘出了圆板位移、应力响应曲线以及冲击力随时间的变化曲线。     

Vibration problems of flexible circular plates with initial deflection

In this paper,the differential equations of flexible circular plates with initialdeflection are derived.The stability of motion is investigated in phase plane.Theperiodical solutions of nonlinear vibration for circular plates with initial deflection areobtained by use of Galerkin method and Lindstedt-Poincare perturbation method.Theeffect of initial deflection on the dynamic behavior of the flexible plates are alsodiscussed.