加筋板架击穿概率分析

为评估攻击武器作用下舰船结构的安全性,对战斗部冲击载荷作用下加筋板架的击穿概率进行分析.取初始撞击速度、战斗部密度、材料的弹性模量和极限强度作为随机变量,利用随机数生成程序得到50组随机变量的初始值;采用有限元程序进行仿真计算,得到战斗部击穿板架后的末速度值,并检验末速度是否服从正态分布,若不服从则利用最大熵法拟合末速度的概率密度函数;考虑战斗部撞击点和板架加强筋的相对位置关系,采用速度破坏准则,利用蒙特卡罗方法模拟得到不同入射角度的战斗部击穿单层和双层加筋板架的概率.该方法所用样本数量少,充分利用了样本信息,效率较高,具有一定实际应用价值.     

光电转台轻量化几何形状优化研究

对光电转台进行轻量化,首先需要进行几何形状进行优化.筋板如何布置才能使转台的动态刚度达到最优,在设计中一直是一个难点.基于此,通过对转台的连接部件、止推轴承及径向轴承进行有效简化,建立起了光电转台的动力学模型,结合模型.对转台内部的筋板布置形式进行了详尽的研究比较.研究结果表明,要想获得满意的动态刚度,单纯地增加筋板数量并不能达到要求,而应该根据其具体的振动情况来选择合理的筋板布置形式,并且在平行于振型方向的筋板上,开孔时的动刚度效果相对地比未开孔时的动刚度效果要好.     

矢跨比对加劲球壳弹性屈曲性能的影响

加劲球壳的承载力取决于整体稳定性。由于加劲球壳属于各向异性壳,影响其屈曲性能的因素较多,至今没有统一的方法获取其整体失稳时的临界荷载。矢跨比是球壳结构屈曲性能分析中的关键因素之一,文中针对矢跨比对加劲球壳弹性屈曲性能的影响进行分析。先利用ABAQUS软件对球面薄壳进行屈曲分析,验证有限元分析的可靠性;再建立跨度恒定矢高变化的加劲球壳的有限元缩尺模型,分析弹性屈曲临界荷载与矢跨比之间的关系。研究结果表明,当环向与经向加劲肋间距比值在2.55-3.65范围内,屈曲临界荷载与矢跨比呈正相关关系。有效地增大矢跨比有利于提高其整体稳定性。     

基于强度稳定综合理论的深海潜器耐压圆柱壳极限强度的解算

通过对弹性基础梁复杂弯曲综合因子N的研究,得以应用强度稳定综合理论的解析法对弹性基础梁复杂弯曲的稳定性进行计算.由于圆柱壳轴对称失效变形的微分方程可化为复杂弯曲的弹性基础梁的微分方程,于是圆柱壳和加肋圆柱壳壳板失稳的临界应力公式也可以由此方法得出.最后通过与高强钢的加肋圆柱壳的实验结果和已有工作比较,证明了强度稳定综合理论方法在圆柱壳结构壳板稳定性计算上的适用性.     

Residual strength prediction of multiple cracked stiffened panels

Prediction of the coalescence of adjacent cracks is critical for residual strength estimation of structures under multiple site damage conditions. A methodology successfully developed for the case of crack link‐up prediction of un‐stiffened plates, is extended for the case of typical cracked stiffened aircraft panels. The proposed link‐up criterion is based on the change in the magnitudes of elastic and plastic strain energies of the stiffened panel, before and after the cracks coalesce. The strain energy magnitudes of interest are calculated using non‐linear elastic–plastic finite‐element analysis. For the application and verification of the method, experimental results from the open literature are used. Residual strength values calculated by the proposed methodology are in good agreement with the experimental results. The present criterion provides superior results when compared to the existing and commonly applied link‐up criteria.     

两端用圆板封口的环肋柱壳振动声辐射性能分析

研究两端用圆板封口的环肋圆柱壳结构在流场中的振动声辐射特性,着重分析了由环肋圆柱壳和端部圆板所围空腔的内部声场对整个系统结构振动和声辐射的影响.基于扩展的Rayleigh-Ritz法,利用Hamilton变分原理推导出圆柱壳与圆板的耦合振动方程.考虑了静水压力的影响,环肋圆柱壳与端部圆板之间采用二自由度弹簧模拟弹性连接的等效刚度.环肋圆柱壳声辐射的研究中,用Helmholtz波动方程和流固交界面上的速度相容条件求得壳体表面辐射声压的表达式,该表达式对有限长圆柱壳进行Fourier积分变换得到壳体外表面辐射声压的解;用Green函数法来求解环肋圆柱壳和端板所围空腔的内部压力场.     

Implementation of a crack propagation constraint within a structural optimization software

A crack propagation constraint related to the stress intensity factor is examined for the minimum-weight design optimization of a composite blade-stiffened panel. A low-fidelity approach uses a closed-form solution for the stress intensity factor, while a high-fidelity approach uses the stress distribution around the crack. Structural optimizations are performed by low- and high-fidelity approaches for a number of panels configured with different values of the load, crack length, and blade height. Response surface (RS) approximations are then constructed for the optimal weight as a function of the three configuration variables. The computational cost, numerical noise, and accuracy for the two approaches are compared. An additional constraint in the low-fidelity solutions is found to be active for some of the configurations, increasing the difference between the low-fidelity and high-fidelity optima. It is shown that outlier analysis helps to identify the configurations with the largest difference.     

航空复合材料短柱加筋板压缩性能试验研究

开展了航空复合材料短柱加筋板的轴向压缩试验。试验件的破坏形式主要包括壁板的撕裂、筋条的断裂和端部的压溃现象,试验过程中,壁板及筋条没有出现明显的脱粘现象。在试验加载初期,载荷-应变曲线呈线性一致的增加趋势,位移测量点的离面位移值基本保持在0 mm附近;当压缩载荷超过临界屈曲载荷时,载荷-应变曲线出现了明显的分岔现象,且离面位移值快速增加。复合材料短柱加筋板失稳后仍然具有后屈曲承载能力,但是该承载能力较小,当短柱加筋板发生失稳后,随着压缩载荷的增加,试验件会很快发生破坏。有限元仿真结果与试验结果较一致,仿真结果表明短柱加筋板主要发生了壁板的局部失稳。     

Nonlinear mechanical,thermal and thermo-mechanical postbuckling of imperfect eccentrically stiffened thin FGM cylindrical panels on elastic foundations

This paper presents an analytical approach to investigate the nonlinear stability analysis of eccentrically stiffened thin FGM cylindrical panels on elastic foundations subjected to mechanical loads, thermal loads and the combination of these loads. The material properties are assumed to be temperature-dependent and graded in the thickness direction according to a simple power law distribution. Governing equations are derived basing on the classical shell theory incorporating von Karman–Donnell type nonlinearity, initial geometrical imperfection, the Lekhnitsky smeared stiffeners technique and Pasternak type elastic foundations. Explicit relations of load–deflection curves for FGM cylindrical panels are determined by applying stress function and Galerkin method. The effects of material and geometrical properties, imperfection, elastic foundations and stiffeners on the buckling and postbuckling of the FGM panels are discussed in detail. The obtained results are validated by comparing with those in the literature..     

局部荷载作用下单向加肋板的弯曲问题

本文用混合型三角级数法,讨论了顺肋边简支单向加肋矩形板,在沿局部矩形域分布的均布荷载、集中力、集中力偶、线分布力、线分布力偶及位于同一线上的等距等值集中力等局部荷载作用下的计算.文中导出了全部内力及位移的解析解,并给出了解决有关工程问題的数值例题.