双基地雷达抗干扰模型的研究

从双基地雷达方程和实施压制性噪声干扰前后所带来的热噪声的变化出发,给出了双基地雷达探测区和干扰暴露区的计算模型,分析计算了在自卫式干扰和远距离支援干扰条件下的双基地雷达抗有源压制性干扰性能,并与单基地雷达情况进行了比较,说明收发分置的双基地体制雷达具有较强的抗干扰能力。给出了仿真算例,结果验证了这种观点。     

火灾场钢筋混凝土简支梁抗弯性能分析

通过对火灾中钢筋混凝土简支梁截面温度场和材料热力学性能分析,将混凝土分为弹性区和塑性区来分别计算其强度,建立了火灾场简支梁截面内混凝土应力和梁极限抗弯承载力的计算公式,通过具体算例分析了钢筋混凝土简支梁截面温度场和极限承载力的变化规律和原因。     

不同腐蚀状态不锈钢管焊缝区 碱性腐蚀的电位噪声特征

利用电化学电位噪声方法检测了不同腐蚀状态304与316两种不镑钢管焊缝区试样在室温碱液中的腐蚀行为,并采用电化学噪声时域谱、频域谱进行了分析,结果表明:不同腐蚀状态焊缝试样的腐蚀电位及噪声时城谱特征不同,可利用电位噪声频城谱的高频斜率K值定性判定是否发生局部腐蚀,同时可根据频城谱中发生事件特殊频率fn区分材料的腐蚀状态...     

舰空导弹协同攻击目标分配方法研究

根据双舰编队反导队形的配置和舰空导弹的战术技术性能,提出了针对多批目标的实时火力分配决策方法,根据当前态势和火力单元特性对需分配的目标进行静态实时火力分配,系统不断循环直至目标分配完毕,最后用实例进行了分析,计算结果表明了该方法的有效性.     

角度闪烁干扰对地空导弹火力拦截能力的影响

角度闪烁干扰对地空导弹火力拦截能力的影响,是电子对抗部队迫切需要解决却又缺乏系统研究的难题。为解决这一难点问题,首先在研究杀伤区纵深和掩护扇区受干扰变化的基础上,分析了双机闪烁干扰对地空导弹射击目标脱靶量及射击次数的影响,然后建立了角度闪烁干扰条件下地空导弹对目标的合成杀伤概率计算模型,最后通过算例验证模型的有效性,得出了具有实用价值的结论,可为空袭作战中作战效能评估提供参考。     

■AB■_n型嵌段聚氨酯软硬段间的相容性与动态力学谱

本文讨论了■A—B■_n丢嵌段聚氨酯软硬段间的相容性对其动态力学谱(tanσ曲线)的影响,指出:相容性对tanσ曲线的影响的本质是相间过渡区的性质。对■A—B■_n型嵌段聚氨酯体系,当其由完全不相容向完全相容(或由完全相容向完全不相容)变化时,tanσ曲线形状的变化为窄→宽→窄。通过tanσ曲线的变化可定性分析其相容性变化。     

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。     

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。     

夺占小型岛屿作战综合登陆舰编队展开点选择优化模型

针对综合登陆舰编队夺占小型岛屿作战中的威胁特点,确定了岸基航空兵对综合登陆舰的有效掩护区,建立了综合登陆舰展开点选择的优化模型,并给出了简单方便的图上作业法,为合理确定综合登陆舰的展开点提供了方法和依据。     

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.