复合材料层合结构的非线性传热分析

基于一阶热层合理论,考虑材料非线性的影响,建立了复合材料层合结构非线性传热分析的热层合理论及其有限元方程.通过数值算例研究了材料非线性对反对称复合材料层合板瞬态温度场的影响.     

复合材料新的热层合理论及其有限元方法研究

本文基子三维各向异性热传导方程和复合材料的一般层合理论,推导出复合材料层合结构瞬态温度场分析的新的热层合理论,并依据此理论建立了简单、实用的有限元格式。数值算例表明：基于热层合理论的有限元方法有较好的精度,同时又比传统的分析方法更简便、有效。     

复合材料层合圆柱壳的动力响应与层间应力

采用分层壳理论和厚度方向的二次插值函数推导出正交铺设层合圆柱壳的动力响应方程,并得出简支层合圆柱壳自由振动问题的解.对于给定算例,计算出的自振频率与三维分析的结果吻合良好,说明所推导的二维解具有足够精度.计算了前四阶模态对应的壳中应力.计算结果说明,对于高阶模态,层间应力相对于面内应力的比值远高于低阶模态的对应比值,高的层间正应力是高阶模态导致脱层破坏的主要原因.     

策略不确定条件下基于高阶超博弈的军事对抗决策方法

军事对抗决策中面临的一个主要问题是难以确定敌方的策略集。基于超博弈分析策略不确定条件下的军事对抗决策问题。在分析超博弈中信念迭代原理的基础上,提出了基于高阶超博弈的对抗决策方法。将高阶信念中的结果反思到低阶信念,并最终反思到一阶信念中,将己方的决策建立在对敌方可能决策的分析的基础上。使得己方的决策具有针对性且更加合理。以二战中西线战役为例验证了方法的可行性和有效性。     

基于区间数理论的空战目标威胁评估

针对空战目标威胁评估问题,提出了一种新的基于区间数理论的评估方法。在分析了现有的目标威胁评估方法中距离威胁模型存在不足的基础上,提出了改进的距离威胁模型。给出了区间数特征向量法求解威胁指标权重的计算步骤,建立了基于区间数理论的空战目标威胁评估的数学模型。最后给出了仿真算例,仿真结果表明该方法是合理和有效的。     

基于D-S证据理论的技术成熟度评估关键技术识别方法研究

针对技术成熟度评估中识别关键技术这一多属性群决策问题,提出了采用证据理论的一种新方法,解决了由于专家意见具有发散性和冲突性而导致的意见难以合成的问题．通过引入和分析不确定度的概念和含义,给出新的不确定度的计算方法,有效地解决了评价中的证据冲突问题．最后通过一个算例给出了应用的步骤和方法．     

基于灰色关联分析的反导导弹战斗部作战效能评估

针对反导导弹战斗部的性能特点,以灰色关联理论为基础,采用灰色加权关联度分析进行综合评判,建立了反导导弹战斗部作战效能评估模型．最后通过算例,验证了该模型的完整性,最终为决策者做出合理的作战决策提供了理论参考．     

基于四阶累积量切片谱的谐波信号线谱提取

提出一种新的谐波信号线谱提取方法,通过对四阶累积量对角切片或非对角切片作傅立叶变换,得到四阶累积量切片谱,运用切片谱提取谐波信号的线谱特征。相比于传统的基于高阶谱估计的线谱提取方法,该方法既继承了其消除高斯噪声的优点,又简化了计算量、提高了估计质量,并且不再要求信号满足二次或三次相位耦合。仿真实验证明了该方法的有效性和优越性。     

WCNS格式在热化学非平衡流数值模拟中的应用研究

高精度格式因其在较低的计算资源消耗下仍能保持足够的精度而在精细流动结构的模拟中具有独特优势。首次将显式5阶加权紧致非线性格式(WCNS-E-5)引入二维高温非平衡流计算。进行了自由流速度5.0~5.7km/s的高焓风洞和高空条件下的圆柱非平衡流场数值模拟,得到了正确的流场参数分布,壁面压力和壁面热流等结果与实验值吻合较好。计算结果表明WCNS-E-5格式较2阶的MUSCL格式具有更好的热流网格收敛特性。分析并针对算例条件初步解决了高阶格式在刚性化学反应流模拟中的鲁棒性问题,为进一步采用高阶格式开展流场结构更加复杂的热化学非平衡流数值研究奠定了良好基础。     

加权紧致非线性格式在热化学非平衡流数值模拟中的应用

高精度格式因其在较低的计算资源消耗下仍能保持足够的精度而在精细流动结构的模拟中具有独特优势。将显式5阶加权紧致非线性格式(WCNS-E-5)引入二维高温非平衡流计算,进行自由流速度5.0~5.7 km/s的高焓风洞和高空条件下的圆柱非平衡流场数值模拟,得到正确的流场参数分布、壁面压力和壁面热流等结果与实验值吻合较好。计算结果表明,WCNS-E-5格式较2阶的MUSCL格式具有更好的热流网格收敛特性。分析并针对算例条件初步解决了高阶格式在刚性化学反应流模拟中的鲁棒性问题,为进一步采用高阶格式开展流场结构更加复杂的热化学非平衡流数值研究奠定了良好基础。     

剪刀撑水泥砂浆网薄层加固砌体墙体拟静力试验

主拉应力破坏是砌体结构在地震荷载作用下最常见的一种破坏形式,剪刀撑水泥砂浆网薄层加固法就是针对砌体结构抵抗主拉应力不足的一种加固方法。为了考察该方法加固砌体墙体的受力性能及加固效果,对6片砂浆强度不同、加固方法不同的墙体试件进行了拟静力试验。试验结果表明：剪刀撑水泥砂浆网薄层加固法能够明显提高砌体墙体的抗剪承载力;该方法更适合于加固砂浆强度较低的砌体墙体;采用该方法加固后的砌体墙体破坏形式以剪切滑移破坏为主;加固面层能够与原有墙体较好地共同工作。目前剪刀撑水泥砂浆网薄层加固法是一个崭新的课题,该拟静力试验给出的试验分析结果和建议可供相关研究和加固工程设计参考。     

Texture evaluation in AZ31/AZ31 multilayer and AZ31/AA5068 laminar composite during accumulative roll bonding

This article presents the texture development of magnesium AZ31 alloy in the accumulative roll bonded (ARB) AZ31/AZ31 multilayer and AZ31/AA5086 laminate composite. The comparative study demonstrates that the texture evolution in AZ31 in a multilayer system is strongly influenced by the interfaces. A typical basal texture of AZ31 has been observed in AZ31/AZ31 multilayer with texture intensity increased with the rolling deformation. Presence of AZ31/AA5086 interface in the laminate composite leads to a tilted basal texture along the rolling direction (RD) in AZ31 alloy. The texture intensity of composite increased initially with rolling reduction and weakened at the higher rolling strain. Weakening of texture in AZ31 during the laminate processing at higher strain has been attributed to the development of wavy interfaces in AZ31/AA5086 laminate.     

Development of cost effective personnel armour through structural hybridization

The objective of the present study is to develop cost effective thermoplastic hybrid laminate using Dyneema® HB50 and Tensylon®HSBD 30A through structural hybridization method. Laminates having 20 mm thickness were fabricated and subjected to 7.62 × 39 mm mild steel core projectile with an impact velocity of 730 ± 10 ms⁻¹. Parameters such as energy absorption, back face deformation and rate of back face deformation were measured as a function of hybridization ratio. It was observed that hybrid laminate with 50:50 ratio (w/w) of Tensylon® and Dyneema® with Tensylon® as front face showed 200% more energy absorption when compared to 100% Tensylon® laminate and showed equal energy absorption as that of expensive 100% Dyneema® laminate. Moreover, hybrid laminate with TD50:50 ratio showed 40% lower in terms of final back face deformation than Dyneema® laminate. Rate of back face deformation was also found to be slow for hybrid laminate as compared to Dyneema® laminate. Dynamic mechanical analysis showed that, Tensylon® laminate has got higher stiffness and lower damping factor than Dyneema® and hybrid laminates. The interface between Tensylon® and Dyneema® layers was found to be separating during the penetration process due to the poor interfacial bonding. Failure behaviour of laminates for different hybridization ratios were studied by sectioning the impacted laminates. It was observed that, the Tensylon® laminate has undergone shear cutting of fibers as major failure mode whereas the hybrid laminate showed shear cutting followed by tensile stretching, fiber pull out and delamination. These inputs are highly useful for body armour applications to design cost effective armour with enhanced performance.     

多轴向织物层合板层间剪切强度有限元分析与实验研究

用VIMP工艺制备了UD、0/45/-45、0/45/90/-45三种多轴向织物增强,四种厚度的GFRP层合板试样,采用短梁剪切实验考察了层间剪切强度和破坏模式。建立了GFRP层合板短梁剪切试样有限元模型,计算了内部层间剪应力分布。结合计算和实验结果分析表明层合板存在由宽度方向层间剪应力变化导致的自由边缘效应,含偏轴铺层的层合板更容易发生边缘开裂破坏。厚度相同时0/45/-45多轴向织物增强层合板的层间剪切强度最高。短梁剪切强度测试存在尺寸效应,随着厚度的增加,强度下降,样品波动系数增大。     

Low velocity impact studies of E-glass/epoxy composite laminates at different thicknesses and temperatures

Low velocity impact experiments were carried out on E-glass/epoxy composite laminates having varying thicknesses at sub zero and elevated temperatures using hemi spherical steel impactor of 16 mm diameter with impact energies in the rage of 50–150 J. The performance of the laminates was assessed in terms of energy absorption, maximum displacement, peak force and failure behaviour. Results indicated that the effect of temperature on energy absorption of the laminate is negligible although the laminates are embrittling at sub zero temperatures. However it has influence on failure behaviour and displacement. Peak force has increased linearly with increase in laminate thickness from 5 to 10 mm. However it got reduced by 25% when temperature was increased from −20 °C to 100 °C. Based on experimental results, laminate perforation energies were predicted using curve fitting equations. Statistical analysis was carried out using Taguchi method to identify the global effects of various parameters on laminate performance and confirmed that the laminate thickness has significant influence as compared to temperature, for the studied range.     

Prediction of three-dimensional elastic behavior of filament-wound composites based on the bridging model

This work provides a method to predict the three-dimensional equivalent elastic properties of the filament-wound composites based on the multi-scale homogenization principle.In the meso-scale,a representative volume element(RVE)is defined and the bridging model is adopted to establish a theoretical predictive model for its three-dimensional equivalent elastic constants.The results obtained through this method for the previous experimental model are compared with the ones gained respec-tively by experiments and classical laminate theory to verify the reliability of this model.In addition,the effects of some winding parameters,such as winding angle,on the equivalent elastic behavior of the filament-wound composites are analyzed.The rules gained can provide a theoretical reference for the optimum design of filament-wound composites.     

剪刀撑水泥砂浆网薄层加固低强度砂浆砖砌体拟静力试验

对低强度砂浆砖砌体墙片经过剪刀撑水泥砂浆网薄层加固后,与未加固砌体墙片在相同竖向压应力下进行拟静力对比试验。试验结果表明,对于砂浆强度很低的砌体,剪刀撑水泥砂浆网薄层加固能有效增强砌体的抗震性能,其极限荷载、极限位移、抗侧刚度均比未加固墙体有明显提高,延性比有所降低。在此基础上讨论了剪刀撑水泥砂浆网薄层加固砌体结构墙体的抗剪承载力计算模型,并提出了抗剪承载力建议公式,公式值与试验值符合较好。结论可为公程设计人员提供参考依据。     

FECL100K组件在强迫风冷下的热传递模型

文中运用传热学理论,用电模拟法建立了FECL100K24线陶瓷扁平封装组件在强迫风冷条件下的等效热路,并在此基础上推算出其热传递数学模型,为电子计算机辅助热设计提供了基础。文中还运用所建立的等效热路和数学模型,对该组件在电子设备中安装形式的合理性进行了论证。