陶瓷基复合装甲防12.7mm穿甲燃烧弹的靶试研究（Ⅱ）

基于对材料特性和防弹机理的认识,设计了由（SiC＋Si）陶瓷、616装甲钢和高强PE材料构成的陶瓷基复合靶板,靶板防护面密度为118 kg/m2,尺寸为500 mm×500 mm×25 mm。利用现役12.7 mm穿甲燃烧弹考核靶板在6发弹打击下的防护能力,检验靶板设计思路。结果表明：靶板结构是可行的,可防住V25为818 m/s的现役12.7 mm穿甲燃烧弹。     

Bending and stress analysis of polymeric composite plates reinforced with functionally graded graphene platelets based on sinusoidal shear-deformation plate theory

The bending and stress analysis of a functionally graded polymer composite plate reinforced with gra-phene platelets are studied in this paper. The governing equations are derived by using principle of virtual work for a plate which is rested on Pasternak's foundation. Sinusoidal shear deformation theory is used to describe displacementfield. Four different distribution patterns are employed in our analysis. The analytical solution is presented for a functionally graded plate to investigate the influence of important parameters. The numerical results are presented to show the deflection and stress results of the problem for four employed patterns in terms of geometric parameters such as number of layers, weight fraction and two parameters of Pasternak's foundation.     

A comprehensive review on material selection for polymer matrix composites subjected to impact load

Polymer matrix composites (PMC) are extensively been used in many engineering applications. Various natural fibers have emerged as potential replacements to synthetic fibers as reinforcing materials composites owing to their fairly better mechanical properties, low cost, environment friendliness and biodegradability. Selection of appropriate constituents of composites for a particular application is a tedious task for a designer/engineer. Impact loading has emerged as the serious threat for the composites used in structural or secondary structural application and demands the usage of appropriate fiber and matrix combination to enhance the energy absorption and mitigate the failure. The objective of the present review is to explore the composite with various fiber and matrix combination used for impact applications, identify the gap in the literature and suggest the potential naturally available fiber and matrix combination of composites for future work in the field of impact loading. The novelty of the present study lies in exploring the combination of naturally available fiber and matrix combination which can help in better energy absorption and mitigate the failure when subjected to impact loading. In addition, the application of multi attributes decision making (MADM) tools is demonstrated for selection of fiber and matrix materials which can serve as a benchmark study for the researchers in future.     

复合土钉支护的有限元分析

复合土钉支护是从土钉墙的基础上发展起来的,它在一定程度上克服了土钉墙的缺点,是一种应用更加广泛的基坑支护新技术。通过建立有限元模型模拟了水泥土桩复合土钉墙的分步开挖与支护的过程,比较了复合土钉支护与土钉支护在土体位移、地表沉降、基底隆起及超挖引起的破坏形态的不同,研究了复合土钉支护的作用机理。结果表明:复合土钉支护能够充分调动周围土体共同作用,更加有效的控制了基坑变形,其支护效果明显优于一般的土钉支护。     

电刷镀含纳米粉复合镀层结构和磨损性能

用含纳米金刚石粉的镍镀液电刷镀复合镀层,系统试验研究了复合镀层中纳米金刚石对镀层显微结构、力学性能及耐磨性能的影响.结果表明,纳米金刚石的弥散强化作用,可有效改善镀层的生长、减小内应力,提高镀层的显微硬度.含纳米金刚石粉的复合镀层在室温、高负荷下具有优良的抗疲劳和抗磨损性能,其耐磨性是纯镍镀层的4倍.     

传感器与综合火控系统组网的协同作战能力系统

协同作战能力(CEC)系统是美国海军最早使用的与传感器和武器系统组合的网络中心战系统之一.简要介绍了CEC的发展背景,较系统地阐述了传感器组网和综合火控的概念.同时还介绍了CEC系统的配置和复合识别能力,指出CEC用作联合传感器网络基础的可能性.最后,展望了未来先进的传感器网络,并指出了在CEC中发挥网络优势必须解决的两个难题.     

整体缝合夹芯结构复合材料力学性能

所设计的新型整体缝合泡沫夹芯复合材料结构,能够避免一般斜缝方式引起纤维交叉损坏的弊端。采用真空导入模塑工艺制备整体缝合泡沫夹芯结构复合材料,研究缝合结构、缝合方式以及缝合纱线用量对整体缝合泡沫夹芯复合材料平压力学性能和弯曲性能的影响。结果表明,新型缝合结构在保证平压力学性能的同时,相比于垂直缝合结构弯曲破坏载荷提高了94.4%;穿透缝合方式能够显著提高试样的平压强度和弯曲破坏载荷;随着缝合纱线用量的增加,整体缝合泡沫夹芯复合材料的压缩和弯曲性能显著提高。     

一种新的复合导引头多源异步信息融合精确拦截算法

针对单一制导体制难以满足现代战场作战需求,而多传感器数据更新率不同步的问题,建立一种新的微惯导/毫米波/红外复合制导体制,研究了该体制下多传感器异步信息融合的时间同步和空间配准问题;提出一种自适应Unscented卡尔曼滤波算法,该算法采用预测残差构造状态模型误差统计量,通过自适应因子调整状态模型信息对状态参数估值的贡献,有效控制状态模型噪声异常对状态参数估值的影响。将提出的算法应用到微惯导/毫米波/红外复合制导系统中进行仿真验证,结果表明,提出的自适应Unscented卡尔曼滤波算法的解算精度高于标准扩展卡尔曼滤波和Unscented卡尔曼滤波算法,能有效提高导弹的制导的解算精度。     

改性C/C复合材料快速制备与抗烧蚀性能考核

采用液相浸渍法结合反应熔渗法快速制备改性C/C复合材料,研究其微观组织及在氧乙炔焰和高频等离子体风洞环境中的烧蚀行为。结果表明:改性C/C复合材料主要含有Hf C,Zr C,Ta C等高熔点陶瓷改性相,其密度为3.83 g/cm3,开孔率仅为4.71%。氧乙炔焰烧蚀360 s后,改性C/C复合材料表面形成一层主要由Hf O2,Zr O2,Ta2O5组成的致密氧化物层,材料的线烧蚀率为0.005 18 mm/s。使用高频等离子体风洞考核改性C/C复合材料球头模型,在热流量3.5 MW/m2、驻点温度2293℃的条件下考核180 s后,模型表面生成致密光滑的氧化物保护层,与基体结合牢固,模型形状及尺寸无明显改变,去掉氧化物后测得其线烧蚀率为0.001 72 mm/s。     

复合导引头多源异步信息融合精确拦截算法

针对单一制导体制难以满足现代战场作战需求且多传感器数据更新率不同步的问题,建立一种新的微惯导/毫米波/红外复合制导体制,研究了该体制下多传感器异步信息融合的时间同步和空间配准问题;提出一种自适应无迹卡尔曼滤波算法,该算法采用预测残差构造状态模型误差统计量,通过自适应因子调整状态模型信息对状态参数估值的贡献,有效控制状态模型噪声异常对状态参数估值的影响。将提出的算法应用到微惯导/毫米波/红外复合制导系统中进行仿真验证,结果表明,提出的自适应无迹卡尔曼滤波算法的解算精度高于标准扩展卡尔曼滤波和无迹卡尔曼滤波算法,能有效提高导弹的制导的解算精度。