含有分层损伤的复合材料加筋层合板的屈曲性态研究

基于Ｍｉｎｄｉｎ假定推导了考虑剪切的复合材料加筋层板的有限元列式,并在此基础上计算出筋间基板含嵌入分层以及筋与基板连接处含穿透分层的加筋层合板在受压缩载荷情况下的屈曲模式和临界力。本文所给出的有限元方法及结论对从事复合材料结构设计的工程人员具有参考价值。     

水下爆炸载荷作用下加筋板的毁伤模式

为研究加筋板结构在水下爆炸载荷作用下的破坏模式,进行了一系列模型试验。通过对试验结果的分析,将加筋板的毁伤模式总体分为塑性大变形（模式I）、拉伸破坏（模式II）和剪切破坏（模式III）等3大类。又根据载荷强弱和加强筋的相对强度,将每种破坏模式细分为3种子模式。提出了一个量纲一的损伤因子,作为预报毁伤模式的判据。     

CFRP加筋板剪切稳定性试验和数值分析模型研究

为研究数值模型对碳纤维增强复合材料(CFRP)加筋板面内剪切稳定性试验计算结果的影响,采用画框式夹具对CFRP加筋板进行了屈曲试验,获得了初始屈曲载荷和载荷-应变曲线;同时基于ABAQUS有限元软件建立了四种数值模型,分别进行线性屈曲和非线性屈曲分析,通过将计算结果与试验结果的比较,确定了有效的数值模型．在此基础上,通过对屈曲前、后有效区边界上的内力分布的比较分析,明确了夹具的传力效果、试件真实的受力状态,以及偏差产生原因．     

Propagation behaviour of guided waves in tapered sandwich structures and debonding identification using time reversal

Fundamental symmetric and anti-symmetric Lamb wave modes are characterised in terms of their velocity and magnitude variation as they encounter a gradual change in the thickness of a composite sandwich plate with a high density foam core (Dyvinicell HP100). Wave mode selection is optimised to enhance the sensitivity of guided waves for debonding inspection of tapered sandwich structures, and the conversion in wave modes after interaction with the taper is also studied. A taper change in the sandwiched structure can induce a clear change in the wave magnitude when the guided waves are excited at relatively low frequency (below around 150 kHz), while there is less effect on the velocity of the propagating waves. The effect of the taper on the signal magnitude and velocity is reduced when the excitation frequency is increased beyond 200 kHz. An imaging algorithm based on time reversal is developed to detect multiple debonding in tapered composite sandwich panels, using guided waves at different excitation frequencies ranging from 150 to 200 kHz, from an active sensor network. Correlation coefficients between the original and reconstructed time reversal signals are calculated to define a damage index for individual sensing paths, which are subsequently used in a fusion process to identify the presence of multiple debonded areas.     

微波消解-原子吸收光谱法测定人造板饰面材料中铅镉铬

用微波消解作为样品前处理,选择硝酸和过氧化氢为消解试剂,用火焰原子吸收法和石墨炉原子吸收法,可测定三聚氰胺浸渍胶膜纸、聚氯乙烯(PVC)薄膜、漆膜等人造板饰面材料中的铅、镉、铬元素含量。火焰原子吸收法的铅、镉、铬元素检出限分别为0.12,0.020 9和0.146 μg·mL-1;石墨炉原子吸收法的镉元素检出限为0.157 μg·L-1。铅元素相对标准偏差为0.8%～3.0%,加标回收率为94%～109.2%;镉元素相对标准偏差为0.8%～2.1%,加标回收率为94%～106.4%;铬元素相对标准偏差为1.8%～4.9%,加标回收率为98.8%～107.7%。方法准确可靠,适用于人造板饰面材料中重金属的分析,可为制定相关检测方法标准提供依据。     

考虑不确定性因素的有限元屈曲模型验证

研究了考虑不确定性因素的有限元屈曲模型验证和确认方法,提出了不确定参数选择的相关性和敏度分析方法以及基于面积度量的模型评估方法.针对化铣整体壁板,开展了有限元屈曲模型验证研究,首先利用8件试验件,获得了壁板屈曲载荷的试验值,然后依据试验加载情况,建立了考虑试验台的壁板有限元模型,最后利用面积度量方法对有限元模型进行了验证和确认.本文的模型验证和确认方法可为其他工程结构开展类似的工作提供借鉴.     

Numerical analysis of delamination growth for stiffened composite laminated plates

A study of postbuckling and delamination propagation behavior in delaminated stiffened composite plates was presented. A methodology was proposed for simulating the multi-failure responses, such as initial and postbuckling, delamination onset and propagation, etc. A finite element analysis was conducted on the basis of the Mindlin first order shear effect theory and the von-K6rm~n nonlinear deformation assumption. The total energy release rate used as the criteria of delamination growth was estimated with virtual crack closure technique (VCCT). A self-adaptive grid moving technology was adopted to model the delamination growth process. Moreover, the contact effect along delamination front was also considered during the numerical simulation process. By some numerical examples, the influence of distribution and location of stiffener, configuration and size of the delamination, boundary condition and contact effect upon the delamination growth behavior of the stiffened composite plates were investigated. The method and numerical conclusion provided should be of great value to engineers dealing with composite structures.     

含多椭圆孔(核)复合材料加筋层板的应力集中研究

基于各向异性体平面弹性理论中的复势方法,应用杂交变分原理建立了一种与常规有限元相协调的含任意椭圆核各向异性板杂交应力有限元,采用该杂交应力有限元来描述层板的椭圆核区域,采用杆单元来描述加强筋(杆单元的刚度取为层板沿筋条方向的刚度),其余区域采用常规8节点等参单元进行模拟,建立起分析含多椭圆核复合材料加筋壁板问题的力学分析方法,详细讨论了椭圆核大小、位置、筋条尺寸、相对位置、铺层比例等诸参数的影响规律,得到了一些有益的结论。     

激光辐照下圆柱壳结构的稳定性分析

针对航天工程中常用的承受轴压作用的薄壁圆柱壳,分别采用解析方法与特征值屈曲有限元方法分析了圆柱壳结构在均匀轴压作用下的稳定性能,得到了屈曲承载力.并进行了对比,验证了有限元模型的合理性.采用线性屈曲特征值有限元方法分析了强激光辐照作用下圆柱壳的稳定性能,分析表明激光辐照导致壳体局部温度上升并由此带来材料参数的改变,是因为激光辐照在壳体中引起了热应力与热应变,使轴压圆柱壳的屈曲承载力明显降低.论文还着重对加筋圆柱壳结构的稳定性进行了研究,数值分析结果表明,加筋能有效提高圆柱壳结构的抗压承载力,激光辐照作用下,加筋对轴压作用下圆柱壳的屈曲承载力的提高作用更为明显.     

Influence of compression-bending coupling on the stability behavior of anisotropic laminated panels

IntroductionLaminatedplatesandpanelsmadeofadvancedfiber-reinforcedcompositematerialsareincreasinglyusedinstructuralapplicationsbecauseoftheirhighspecificstrengthandspecificstiffness.However,theanalysisoftheselaminatedsimctUresismoredifficultthanthatofthetraditionalisotropicandorthotropicplatesandpanelssinceelasticcouplingsareintroducedintOthemechanicalbehavior.ThiscomplexityincreasesfurtherifunsymmetricIndnatedplatesandpanelsareemployed,sinceamorecomplicatedtheorywithbending-stretchingcouplin…