试论公安现役高等院校办学特色

办学特色是高等学校生存发展的前提和办学优势的集中体现,也是形成核心竞争力的关键。公安现役高等院校突出办学特色,要着力创新办学理念,强化学科专业特色和人才培养特色。     

速变信号的小波分析应用研究

遥测速变参数处理方法大多基于经典分析方法,文中采用现代时频分析方法对遥测动态环境参数进行分析,对比算法在瞬态信号成分检测方面的优势,小波变换比傅立叶变换更适合分析非平稳信号,尤其是含瞬态或突变成分的信号.     

要地防空作战中空中目标威胁度估计的数学模型

为了准确有效地判断敌空中目标的威胁程度,运用层次-效用方法,对要地防空作战中空中目标威胁度建立数学模型。先用层次分析法建立影响因素诸指标的层次结构,然后导出指标因素的效用函数,对其加权和线性变换,得到目标威胁度。该模型使复杂的问题条理化,操作性强,便于计算机辅助决策,为防空指挥员对空情威胁做出正确判断提供了科学依据。     

装备战损等级评定方法研究

在对战场抢修力量部署进行思考的基础上,分析了战损等级评定影响因素,研究了兼顾装备损伤程度与战场抢修力量设置的战损等级评定方法。从而为装备战场抢修任务分工,以及对损伤装备的处理决断提供了依据,并为开展广泛深入的战损等级评定研究奠定了基础。     

气溶胶灭火装置在工业供电系统中的应用

分析工业供电系统的火灾特点和原因 ,结合部分工程实例和气溶胶灭火装置的特性 ,提出该类产品在工业供电系统应用中的优势和施工中的注意事项 ,并展望其应用前景     

基于专家系统的飞机致命性部件辨识方法研究

介绍了飞机致命性部件的辨识方法,尤其对该方法的核心部分,即损伤模式影响及致命性分析(DMECA)进行了详细的剖析。引用可靠性分析中比较成熟的FMECA(故障模式影响及致命性分析)思路来确定飞机的致命性部件,从而可为飞机易损性评估及战伤修复提供前提条件。通过考虑影响部件损伤率的因素(部件的尺寸大小、防护与遮挡、复杂程度等),借助系统综合评价中的关联矩阵方法,解决了DMECA分析表单中损伤率的来源问题,从而使DMECA方法切实可行。     

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.     

Research on the influences of confining pressure and strain rate on NEPE propellant: Experimental assessment and constitutive model

In order to study the influences of confining pressure and strain rate on the mechanical properties of the Nitrate Ester Plasticized Polyether (NEPE) propellant, uniaxial tensile tests were conducted using the self-made confining pressure system and material testing machine. The stress-strain responses of the NEPE propellant under different confining pressure conditions and strain rates were obtained and analyzed. The results show that confining pressure and strain rate have a remarkably influence on the mechanical responses of the NEPE propellant. As confining pressure increases (from 0 to 5.4 MPa), the maximum tensile stress and ultimate strain increase gradually. With the coupled effects of confining pressure and strain rate, the value of the maximum tensile stress and ultimate strain at 5.4 MPa and 0.0667 s⁻¹ is 2.03 times and 2.19 times of their values under 0 MPa and 0.00333 s⁻¹, respectively. Afterwards, the influence mechanism of confining pressure on the NEPE propellant was analyzed. Finally, based on the viscoelastic theory and continuous damage theory, a nonlinear constitutive model considering confining pressure and strain rate was developed. The damage was considered to be rate-dependent and pressure-dependent. The constitutive model was validated by comparing experimental data with predictions of the constitutive model. The whole maximum stress errors of the model predictions are lower than 4% and the corresponding strain errors are lower than 7%. The results show that confining pressure can suppress the damage initiation and evolution of the NEPE propellant and the nonlinear constitutive model can describe the mechanical responses of the NEPE propellant under various confining pressure conditions and strain rates. This research can lay a theoretical foundation for analyzing the structural integrity of propellant grain accurately under working pressure loading.     

Fatigue crack propagation in a helicopter component subjected to impact damage

Damage tolerant methodology is increasingly used in aeronautical components,especially due the fact that the Aviation Regulation requires such an assessment in case an accidental damage occurs.At pre-sent,there is a strong and actual interest in applying such procedures to helicopter components that are subjected to high frequency cyclic loads.In this paper,an investigation on a damaged transmission shaft for a tail rotor transmission of an actual helicopter has been carried out focusing on the fatigue crack propagation.A complete sequence of experimental tests was performed in order to create an actual ballistic damage and to subsequently check the damage tolerant behaviour.The shaft was damaged by oblique ballistic impact and was subsequently subjected to torsional fatigue loading.During the fatigue cycles several cracks propagated from the ballistic damages.Both of these steps(impact and fatigue loading)were also simulated by a complex modelling approach based on Finite Element Models and fracture mechanics theory.The comparison between the experimental and numerical results shows a good agreement but it underlines the need for a very refined modelling technique capable to replicate all the features associated with the damage in order to reliably simulate the subsequent propagation phase.