薄壁结构多层级并发加筋拓扑优化研究

新一代航天装备的主承力薄壁舱段在追求极致轻量化的同时,还具有更高的刚度和抗屈曲等设计指标.传统结构形式和设计方法难以满足轻质高承载的设计要求.为此,本文提出了一种薄壁结构多层级并发加筋拓扑优化方法,通过构建主层级稀疏加筋和次层级密集点阵增强结构整体和局部力学性能,扩展结构设计空间,有效提升材料利用率.其中,主层级加筋布...     

Buckling and postbuckling of stiffened cylindrical shells under axial compression

Buckling and postbuckling behaviors of perfect and imperfect,stringer andorthotropically stiffened cylindrical shells have been studied under axial compression.Based on the boundary layer theory for the buckling of thin elastic shells suggested in ref.[1],a theoretical analysis is presented.The effects of material properties of stiffeners andskin,which are made of different materials,on the buckling load and postbuckling behaviorof stiffened cylindrical shells have also been discussed.     

复合材料加筋板壳结构的后屈曲强度及破坏分析程序系统

本文介绍适用于复合材料（含各向同性材料）层合加筋板壳结构的后屈曲强度及破坏分析的程序系统（ＣＯＭＰＯＳＳ程序系统）的功能特点、原理和结构，通过一个受压剪载荷作用的加筋层合矩形板的破坏分析，并与试验结果作了比较，说明该程序系统的正确、可靠性     

加筋薄壳结构分析与优化设计研究进展

伴随装备大型化和承载重型化等发展趋势,装备中加筋薄壳结构尺寸越来越大,成型工艺与结构细节也越来越复杂,对结构优化设计的精细程度、新型轻质结构发现和力学性能数值预测精度提出了更高的要求,给复杂板壳非线性分析模型、优化问题的数学建模和求解算法带来新的挑战。本文从加筋壳稳定性分析方法、折减因子确定方法以及考虑几何缺陷的加筋壳设计方法三个方面进行综述,介绍国内外相关研究进展。     

Postbuckling of imperfect stiffened cylindrical shells under combined external pressure and heating

1.IntroductionStiffenedcylindricalshellsarewidelyusedinmanytypesofstructures.Inpracticetheyoftensubjecttovarioustypesofcombinedthermalandmechanicalloadingandmayhavesignificantandunavoidableinitialgeometricalimperfections.Therefore,thepostbucklingbehaviorofimperfectstiITenedcylindricalshellsundercombinedexternalpress.ureandthermalloadingmustbewellunderstood.Manypostbucklingstudieshavebeenmadetbrstiffenedcylindricalshellsunderpureaxialcompression,uniformexternalpressureortheircombinations,where…     

Influence of extra terms on asymptotic analysis of imperfection sensitivity of toroidal shell segment with random imperfection

The bifurcation of a toroidal shell segment with initial imperfection which are subjected to lateral or hydrostatic pressure is studied under the assumption that the initial imperfection are Gaussian random stress-free displacement whose mean and autocorrelation function are given. We use a perturbation scheme developed by Amazigo [Amazigo, J.C., 1971. Buckling of stochastically imperfect columns on nonlinear elastic foundation. Quart. Appl. Math. 403–491]. A simple approximate asymptotic expression is obtained for the bifurcation load for small magnitudes of the imperfection. The result is compared with results obtained earlier under secondary bifurcation analysis for the imperfections in the shape of the buckling mode and the results in the literature, which shows some significant differences as a result of inclusion of extra terms in the buckling equation.     

New matrix method for response analysis of circumferentially stiffened non-circular cylindrical shells under harmonic pressure

Based on the governing equation of vibration of a kind of cylindrical shells written in a matrix differential equation of the first order,a new matrix method is pre- sented for steady-state vibration analysis of a noncircular cylindrical shell simply sup- ported at two ends and circumferentially stiffened by rings under harmonic pressure.Its difference from the existing works by Yamada and Irie is that the matrix differential equation is solved by using the extended homogeneous capacity precision integration ap- proach other than the Runge-Kutta-Gill integration method.The transfer matrix can easily be determined by a high precision integration scheme.In addition,besides the normal interacting forces,which were commonly adopted by researchers earlier,the tan- gential interacting forces between the cylindrical shell and the rings are considered at the same time by means of the Dirac-δfunction.The effects of the exciting frequencies on displacements and stresses responses have been investigated.Numerical results show that the proposed method is more efficient than the aforementioned method.     

Plastic buckling of stiffened torispherical shell

ＰＬＡＳＴＩＣＢＵＣＫＬＩＮＧＯＦＳＴＩＦＦＥＮＥＤＴＯＲＩＳＰＨＥＲＩＣＡＬＳＨＥＬＬＨａｏＧａｎｇ（郝刚）ＺｅｎｇＧｕａｎｇｗｕ（曾广武）ＨａｏＱｉａｎｇ（郝强）（ＲｅｃｅｉｖｅｄＤｅｃ．３０,１９９４：ＣｏｍｍｕｎｉｃａｔｅｄｂｙＰａｎＬｉｚｈ...     

Koiter-boundary layer singular perturbation method for axial compressed stiffened cylindrical shells

I.IntroductionStiffenedandunstiffenedcircularcylindricalshellsfoundwideusesasprimarystructuralcomponentsinunderwatervehicles,offshoreplatformsandotherstructuralconfigurations.Theinitialinvestigationofthebucklingofstiffenedandunstiffenedcircularcylindrical…     

A Donnell type theory for finite deflection of stiffened thin conical shells composed of composite materials

A Donnell type theory is developed for finite deflection of closely stiffened truncatedlaminated composite conical shells under arbitrary loads by using the variational calculusand smeared-stiffener theory.The most general bending-stretching coupling and the effectof eccentricity of stiffeners are considered.The equilibrium equations,boundary conditionsand the equation of compatibility are derived.The new equations.of the mixed-type ofstiffened laminated composite conical shells are obtained in terms of the transversedeflection and stress function.The simplified equations are also given for some commonlyencountered cases.     

The impact torsional buckling of elastic cylindrical shells with arbitrary form imperfection

A perturbation analysis for the impact torsional buckling of imperfective elastic cylindrical shells subjected to a step torque is given..The imperfection is supposed to be small and has arbitrary form.It is shown that only the imperfection which has the shape of static torsional buckling mode could influence the critical step torque.Finally a formula is presented for the critical step torque.     

大型纵向加筋截断锥壳稳定性的半离散分析

如何计算大型纵向加筋截断锥壳的稳定问题，尚未见到有关报导。本文在沿纵向和环向分别采用Ｈｅｒｍｉｔｅ插值和三角级数插值的基础上，建立了几何非线性带筋环单元，进而导出了半离散分析法，并经过实例检验了它的正确与可靠。这样，本文为建立各类工程结构的半离散单元提出了一种新的途径。     

分区样条等参元方法分析加肋轴对称组合壳

本文提出分区样条等参元方法分析加肋轴对称组合壳在静水外压作用下的应力及稳定性。该方法根据母线几何形状、壳板厚度变化及边界约束状况将加肋轴对称组合壳划分为若干个区域，在不同区域采用不同步长的样条等参元进行分析，因而便于对复杂的组合壳进行分析，并可大大减少计算所需自由度数，减少计算工作量，同时计算精度很高，并且易于进行边界约束处理。应用该方法对加肋锥－柱、加肋锥－环－柱组合壳进行了计算，其结果与其它方法计算值及实验值吻合良好。     

弹性体的正则方程和加筋板的固有频率分析

应用弹性力学的Hamilton正则方程理论和其半解析法,为整体加筋板的固有频率分析提出了一种新颖的数学模型. 采用同一种平面元素离散板和加强筋,并分别建立板和加强筋的线性方程组. 考虑到板和加强筋连接界面上应力和位移的连续性,联立板和加强筋的方程得到全结构的方程组和求解固有频率的特征方程. 主要优越性表现为：结构的旋转惯性、剪切变形等都得到了考虑,且不限制结构的板厚度和加强筋的高度. 多个数值实例的收敛分析和结果证明了方法是可靠的. 该方法很容易被修改用来分析加筋壳、加筋压电材料层合板或带有压电材料传感器和驱动器块的板壳问题.     

Imperfection sensitivity of optimal symmetric braced frames against buckling

Imperfection sensitivity characteristics of the non-linear buckling load factors of non-optimal and optimal symmetric frames are investigated. The frames are subjected to symmetric proportional vertical loads. The optimization problem is formulated under constraints on linear buckling load factors. Although the buckling load factors corresponding to sway and non-sway modes coincide at the optimum design, the non-sway-type asymmetric bifurcation point disappears as a result of geometrically non-linear analysis. Therefore, the maximum allowable load factors of perfect and imperfect systems should be determined by assigning displacement constraints. It is shown that quantitative evaluation is possible for imperfection sensitivity and mode interaction based on the higher order differential coefficients of the total potential energy even for frames of which the critical points should be numerically obtained. Numerical examples are presented to show that the properties of the non-sway bifurcation point are similar to those of a symmetric bifurcation point, and the interaction between sway and non-sway modes does not always lead to enhancement of imperfection sensitivity.     

爆炸载荷作用下加筋板的失效模式分析及结构优化设计

通过对爆炸载荷下具有1根加强筋的固支矩形加筋板的有限元模拟,探讨了抗爆加筋板结构优化设计方法,分析了加筋板的失效模式以及加强筋相对刚度和冲击载荷强度对加筋板失效模式的影响,指出了失效模式Ⅰ下的3种变形模态以及失效模式Ⅱ下的2种子失效模式,得到了失效模式Ⅰ下加强筋和加筋板最大挠度的近似计算公式,提出了单根加筋板的两种失效模式的判别条件,并对具有1根加强筋的固支矩形加筋板抗爆结构进行了优化设计。结果表明,通过数值模拟或模型实验可以求得任意加筋板结构由发生塑性大变形到发生破损的临界条件,从而确定抗爆性能最强时加筋板的质量与加强筋横截面尺寸及间距间的关系,实现对抗爆加筋板结构的优化设计。     

基于区域分解的环肋圆柱壳-圆锥壳组合结构振动分析

提出了一种区域分解法来分析不同边界条件下环肋骨圆柱壳-圆锥壳组合结构的振动特性.首先把组合壳体分解为自由的圆柱壳、圆锥壳段;视环肋骨为离散元件,根据肋骨与圆柱壳段之间的变形协调条件,将肋骨的动能和应变能附加于圆柱壳段能量泛函中.然后基于分区广义变分和最小二乘加权残值法将所有分区界面的位移协调方程引入到组合壳体的能量泛函中.圆柱壳段、圆锥壳段位移变量的周向和轴向分量分别采用Fourier级数和Chebyshev多项式展开.以自由-自由、自由-固支和固支-固支边界条件的环肋骨组合壳体为例,采用区域分解法分析了其自由振动及在不同激励下的振动响应.通过与有限元软件ANSYS结果进行对比,发现两种方法计算结果非常吻合,验证了区域分解方法的计算精度和高效性.     

复合材料加筋板极限压缩承载能力可靠性分析

基于Abaqus软件用户子程序,利用渐进失效分析方法对复合材料加筋板极限压缩承载能力进行预测。算例分析表明,对于加筋板1和2,本文方法给出的极限压缩强度与实验结果的误差分别为2.53%和1.68%。在结构可靠性分析过程中,为提高计算效率,利用屈曲载荷与极限压缩强度之间的关系建立功能函数,只需对极限压缩承载能力进行一次分析。对于加筋板1和2,本文方法相对经典可靠性方法的计算误差分别为-1.04%和-1.01%,计算时间仅为经典可靠性方法的1.18%和1.66%。     

分级型放射肋短壳结构集中力扩散优化设计

在航天箭体结构设计中,燃料贮箱因其特殊的连接形式往往受较大的集中力作用。传统的放射肋短壳结构被用来扩散集中力以减小其造成的危害,但实际效果并不理想。本文基于拓扑优化的概念设计,综合实际短壳结构承载环境和可制造性,提出了一种"分级型放射肋"贮箱短壳结构。围绕刚度、强度、减重、稳定性和集中力扩散效果等多种需求,基于NSGA-Ⅱ遗传算法建立了多目标优化问题模型。通过形状和尺寸的协同优化策略,得到多目标优化的最优Pareto解集。通过三层级、两层级、单一层级最优设计与传统均匀放射肋设计的对比,验证了分级型放射肋设计的优势和效果;之后,结合实际工程要求选择合理的设计方案。     

Nonlinear analysis on dynamic buckling of eccentrically stiffened functionally graded material toroidal shell segment surrounded by elastic foundations in thermal environment and under time-dependent torsional loads

The nonlinear analysis with an analytical approach on dynamic torsional buckling of stiffened functionally graded thin toroidal shell segments is investigated. The shell is reinforced by inside stiffeners and surrounded by elastic foundations in a thermal environment and under a time-dependent torsional load. The governing equations are derived based on the Donnell shell theory with the von K′arm′an geometrical nonlinearity,the Stein and McE lman assumption, the smeared stiffeners technique, and the Galerkin method. A deflection function with three terms is chosen. The thermal parameters of the uniform temperature rise and nonlinear temperature conduction law are found in an explicit form. A closed-form expression for determining the static critical torsional load is obtained. A critical dynamic torsional load is found by the fourth-order Runge-Kutta method and the Budiansky-Roth criterion. The effects of stiffeners, foundations, material,and dimensional parameters on dynamic responses of shells are considered.