三维编织复合材料剪切性能分析

根据三维四向编织复合材料的结构特点，提出了刚度合成法预测编织复合材料剪切弹性模量，比较了整体编织试件和裁剪所得试件理论剪切性能差别，分析了三维编织T300／QY9512复合材料的剪切性能随试件沿宽度和厚度两个方向内部单胞数目的变化规律。结果表明，三维编织复合材料剪切弹性模量是与试件尺寸相关的，只有当试件尺寸较大、沿宽度和厚度两个方向内部单胞数目较多时，试件尺寸的影响可以忽略。当沿宽度方向单胞数目较大时，整体编织试件和裁剪所得试件的剪切模量相近。本文还得到了在复合材料板的纤维体积含量不变的情况下，剪切模量随编织角的变化规律。     

三维编织复合材料几何建模及数值分析

论文根据三维编织复合材料的结构特点,把整体结构分为内部单胞、表面单胞和角单胞三种类型的子单胞,考虑空间纤维束的相互扭结和挤压所造成的纤维束的弯曲和截面变形,针对每种类型的子单胞,建立了相应的几何分析模型.引入周期性位移边界条件,建立了材料的弹性性能预报模型,得到了三维编织复合材料的工程弹性常数.通过数值比较可以看出,论文所给出的数值计算结果与实验结果吻合较好,从而验证了本文模型的有效性.     

基于多尺度方法的三维编织C/C复合材料弯曲失效特性分析

为了预测三维编织C/C复合材料的弯曲失效行为,基于多尺度渐进展开理论,结合细观渐进损伤模型,建立了三维编织C/C复合材料宏细观多尺度分析模型。通过商业有限元软件ABAQUS用户子程序UMAT的二次开发,在宏观结构有限元分析中实时调用细观单胞模型进行细观渐进损伤分析,实现了宏细观尺度之间交互式信息传递和多尺度损伤模拟。利用上述模型对三点弯曲载荷下三维编织C/C复合材料梁的渐进损伤和失效过程进行了模拟,预测了梁的载荷-挠度曲线和弯曲强度,并与实验结果进行了对比分析,验证了基于多尺度方法的三维编织C/C复合材料弯曲强度预测模型的有效性,为此类材料及结构失效分析提供了一种手段。     

树脂基三维编织复合材料粘弹性性能的有限元分析

根据材料的细观结构,采用APDL语言分别建立了纤维束和三维编织复合材料两级单胞的参数化几何模型;推导了Prony级数表示的树脂粘弹性本构方程,对模型进行了组分材料参数设置;对纤维束单胞模型进行扫掠式网格划分,对三维编织复合材料单胞模型进行线-面-体式网格划分;对两级单胞模型均施加合理的边界条件,使单胞边界上的位移满足周期性和连续性。以有限元模型为基础,计算了三维编织复合材料的粘弹性能,并给出了材料粘弹性效应随工艺参数变化的规律。计算结果表明:三维编织复合材料编织方向的粘弹性效应随编织角的增大而增强,随纤维体积比的增大而减弱。该结果与已有实验结论一致。     

三维编织复合材料圆柱壳的扭转后屈曲分析

随着三维编织复合材料应用的日益广泛,且由于三维编织复合材料的优异性能是与细观结构密切相关的,深入研究其细观结构显得尤为重要.本文通过研究三维圆型编织中所形成的空间纱线交织结构的特征,给出改进的三胞结构单胞模型,通过单胞的组装和变换,得到编织预制件的整体力学性能模型.基于Reddy高阶剪切变形理论导得广义Krmn型大挠度方程,计及边界层效应,采用奇异摄动法,考虑非线性前屈曲、大挠度和初始几何缺陷的影响,给出三维四向编织复合材料圆柱壳在扭转载荷作用下的严格满足边界条件的大挠度渐近解,讨论了纤维体积含量、编织角和几何参数等因素对圆柱壳屈曲和后屈曲行为的影响.     

纺织结构复合材料力学性能的实验研究

本文通过实验测定了三维编织结构复合材料侧边未切割、受切割和中央钻孔试件的拉伸性能，对比了受切割和未切割纤维对于试件侧边拉伸应变的影响，并且讨论了拉伸失效的机理和原因．发现受切割和钻孔试件的拉伸性能低于未加工试件的性能，受切割侧边的拉伸应变高于未切割侧边的拉伸应变，三维编织结构复合材料的拉伸失效主要由纤维断裂引起的．文中还对三维编织结构复合材料的孔边应力集中现象进行了研究，并进行了深入分析，得到一个重要结论，即四步法复合材料的孔边应力集中系数比传统层板复合材料和金属材料的低．从这个意义上说，三维编织结构复合材料适合于作为含孔结构的连接件．     

三维多向编织复合材料有效弹性模量的细观计算力学分析

编织复合材料性能预报与材料优化设计研究是纺织复合材料研制开发的重要环节,本文在已建立的三维多向编程复合材料单胞几何模型的基础上,研究建立了含多相介质单元的有限元分析方法,结合实例预报了碳／环氧四向编织复合材料的有效性能并和实验结构进行了对比。     

三维四向编织复合材料的拉伸尺寸效应研究

通过对三维四向碳/环氧编织复合材料的拉伸实验,观测了不同几何尺寸的试件的破坏模式和断口形貌,得到了材料在拉伸载荷下不同的破坏机理以及材料的力学性能与试件几何尺寸的相关性,研究表明材料随着内部单胞数量的增加材料的弹性模量递减,而剪切模量和泊松比递增的变化规律,通过体积平均法从理论上预报了材料的弹性性能,预报结果与实验结果相符,实验和理论所获结论为进一步进行材料的刚度和强度预报以及强度准则的建立奠定了必要的实验和理论基础.     

高温下编织复合材料热相关参数识别方法研究

为了获取高温下编织复合材料的准确弹性参数与热膨胀系数,提出一种基于均匀化理论的热相关参数识别方法. 首先,在编织复合材料单胞有限元模型基础上,基于均匀化理论和热弹性理论,施加周期性位移边界条件和温度边界条件,预测编织复合材 料的热弹性相关参数. 然后,考虑到等效过程中编织复合材料应力分布不均匀等因素引起的误差,将复合材料精细模型的热模态数据作为补 充信息,识别编织复合材料热相关参数,对预测的材料参数进行校准. 本文在二维编织结构单胞模型基础上,开展等效预测和识别方法研 究,验证所提出方法的有效性和准确性. 对比等效和识别后热模态的误差,结果表明:本文提出的基于等效预测的参数识别方法,能够 准确识别高温下编织复合材料宏观热相关参数.      

高温下编织复合材料热相关参数识别方法研究

为了获取高温下编织复合材料的准确弹性参数与热膨胀系数,提出一种基于均匀化理论的热相关参数识别方法.首先,在编织复合材料单胞有限元模型基础上,基于均匀化理论和热弹性理论,施加周期性位移边界条件和温度边界条件,预测编织复合材料的热弹性相关参数.然后,考虑到等效过程中编织复合材料应力分布不均匀等因素引起的误差,将复合材料精细模型的热模态数据作为补充信息,识别编织复合材料热相关参数,对预测的材料参数进行校准.本文在二维编织结构单胞模型基础上,开展等效预测和识别方法研究,验证所提出方法的有效性和准确性.对比等效和识别后热模态的误差,结果表明:本文提出的基于等效预测的参数识别方法,能够准确识别高温下编织复合材料宏观热相关参数.     

Preface

This special issue of PARTICUOLOGY is devoted to the first UK-China Particle Technology Forum taking place in Leeds, UK, on 1-3 April 2007. The forum was initiated by a number of UK and Chinese leading academics and organised by the University of Leeds in collaboration with Chinese Society of Particuology, Particle Technology Subject Group （PTSG） of the Institution of Chemical Engineers （IChemE）, Particle Characterisation Interest Group （PCIG） of the Royal Society of Chemistry （RSC） and International Fine Particle Research Institute （IFPRI）. The forum was supported financially by the Engineering and Physics Sciences Research Council （EPSRC） of United Kingdom,     

The 7th International Conference on Fluid Mechanics May 24-27,2015,Qingdao,China

正http://www.icfm7.org First Announcement and Call for PapersThe objective of International Conference on Fluid Mechanics(ICFM)is to provide a forum for researchers to exchange new ideas and recent advances in the fields of theoretical,experimental,computational Fluid Mechanics as well as interdisciplinary subjects.It was successfully convened by the Chinese Society of Theoretical and Applied Mechanics(CSTAM)in Beijing(1987,     

INFORMATION FOR CONTRIBUTORS

Contributions： The Journal, Acta Mechanica Solida Sinica, is pleased to receive papers from engineers and scientists working in various aspects of solid mechanics. All contributions are subject to critical review prior to acceptance and publication.     

Guide for authors

正Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica Sinica.     

基于鲁棒滤波的捷联导引头视线角速度估计方法

针对捷联导引头无法直接获取视线角速度等信息的问题,研究了鲁棒滤波在大气层外飞行器捷联导引头视线角速度估计中的应用。为了建立非线性滤波估计模型,考虑目标视线角速度的慢变特性,采用一阶马尔科夫模型建立了状态方程;推导了视线角速度的解耦模型,并建立了量测方程;考虑到实际应用中存在系统噪声统计特性失准的问题,基于Huber-Based鲁棒滤波方法,设计了视线角速度滤波器,并完成了基于Huber-Based滤波方法和扩展卡尔曼滤波方法的数学仿真。仿真结果表明Huber-Based滤波方法的视线角、视线角速度及视线角加速度估计精度分别达到0.1140'、0.1423'/s、0.0203'/s2,而扩展卡尔曼滤波方法的视线角、视线角速度及视线角加速度估计精度仅分别为0.6577'、0.6415'/s、0.0979'/s~2。仿真结果证明了该方法可以有效地估计出相对视线角速度等信息,并且在非高斯噪声的条件下,依然可获得较高的估计精度,具有一定的鲁棒性。     

Guide for authors

正Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica     

Use specification of multiscale materials for life spanned over macro-, micro-, nano-, and pico-scale

Multiscale material intends to enhance the strength and life of mechanical systems by matching the transmitted spatiotemporal energy distribution to the constituents at the different scale, say—macro, micro, nano, and pico,—, depending on the needs. Lower scale entities are, particularly, critical to small size systems. Large structures are less sensitive to microscopic effects. Scale shifting laws will be developed for relating test data from nano-, micro-, and macro-specimens. The benefit of reinforcement at the lower scale constituents needs to be justified at the macroscopic scale. Filling the void and space in regions of high energy density is considered.Material inhomogeneity interacts with specimen size. Their combined effect is non-equilibrium. Energy exchange between the environment and specimen becomes increasingly more significant as the specimen size is reduced. Perturbation of the operational conditions can further aggravate the situation. Scale transitional functions and/or f_j/j+1 are introduced to quantify these characteristics. They are represented, respectively, by , and (f_mi/ma,f_na/mi,f_pi/na). The abbreviations pi, na, mi, and ma refer to pico, nano, micro and macro.Local damage is assumed to initiate at a small scale, grows to a larger scale, and terminate at an even larger scale. The mechanism of energy absorption and dissipation will be introduced to develop a consistent book keeping system. Compaction of mass density for constituents of size 10⁻¹², 10⁻⁹, 10⁻⁶, 10⁻³ m, will be considered. Energy dissipation at all scales must be accounted for. Dissipations at the smaller scale must not only be included but they must abide by the same physical and mathematical interpretation, in order to avoid inconsistencies when making connections with those at the larger scale where dissipations are eminent.Three fundamental Problems I, II, and III are stated. They correspond to the commonly used service conditions. Reference is made to a Representative Tip (RT), the location where energy absorption and dissipation takes place. The RT can be a crack tip or a particle. At the larger size scales, RT can refer to a region. Scale shifting of results from the very small to the very large is needed to identify the benefit of using multiscale materials.