基于SDAE+Softmax模型的体系贡献率评估方法

战争就是交战双方作战体系之间的对抗.体系贡献率评估是体系建设和分析重点关注的问题,是对作战要素在作战体系中所发挥作用的一种度量.针对体系的复杂系统特性,构建SDAE+Softmax模型对体系效能涌现过程进行建模,模型描述了体系基础指标与任务指标之间的关系.提取Softmax分类器的分类概率相对值作为体系贡献率评估的综合特征指标,量化体系组分改变对体系效能的影响.基于SDAE+Softmax模型的评估方法,为体系贡献率评估提供了全新的思路,是对传统评估方法的突破.     

Design and analysis of a scheme for the naval gun test shell entering the bore

The test shell without projectile belt is widely used in the teaching, inspection and maintenance of modern automatic naval guns. In order to ensure the normal work of each mechanism, it is very important to design the buffer and limit of the test shell during the process of entering the bore. Taking a certain type of medium caliber naval gun as the research object, the design of colloidal fluid damper and cartridge lock was proposed to ensure the reliability of entering the bore and closing the breechblock. By combining the simulation methods of computational fluid dynamics (CFD) and multibody system dy-namic (MBD), it was analyzed whether the structural design can meet the engineering requirements. The research results show that the colloidal fluid damper can dissipate a large amount of kinetic energy of the shell, and the cartridge lock can limit the rebound movement. The combination of the two ensures the smooth process of closing the breechblock. The research provides a design method for the process of the test shell entering the bore, and provides theoretical support for the feasibility of the method.     

Formation and characterization of core-shell CL-20/TNT composite prepared by spray-drying technique

The core-shell 2,4,6,8,10,12-Hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane/2,4,6-Trinitrotoluene (CL-20/TNT) composite was prepared by spray-drying method in which sensitive high energy explosive (CL-20) was coated with insensitive explosive (TNT). The structure and properties of different formulations of CL-20/TNT composite and CL-20/TNT mixture were characterized by scanning electron microscopy (SEM), Transmission electron microscopy (TEM), Laser particle size analyzer, X-ray photoelectron spectroscopy (XPS), X-ray diffraction (XRD), differential scanning calorimetry (DSC), impact sensitivity test and detonation performance. The results of SEM, TEM, XPS and XRD show that ϵ-CL-20 particles are coated by TNT. When the ratio of CL-20/TNT is 75/25, core-shell structure is well formed, and thickness of the shell is about 20–30 nm. And the analysis of heat and impact show that with the increase of TNT content, the TNT coating on the core-shell composite material can not only catalyze the thermal decomposition of core material (CL-20), but also greatly reduce the impact sensitivity. Compared with the CL-20/TNT mixture (75/25) at the same ratio, the characteristic drop height of core-shell CL-20/TNT composite (75/25) increased by 47.6% and the TNT coating can accelerate the nuclear decomposition in the CL-20/TNT composites. Therefore, the preparation of the core-shell composites can be regarded as a unique means, by which the composites are characterized by controllable decomposition rate, high energy and excellent mechanical sensitivity and could be applied to propellants and other fields.     

Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion

The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.     

美军建模与仿真管理特点及启示

美军是世界上唯一建立战争全域模拟仿真体系的军队,其建模与仿真建设高效管理的一些经验值得我军借鉴。本文归纳了美军建模与仿真管理5个方面的特点：高层机构统一领导,专职部门实施管理,以促进协作和共享为重点,规范化管理,模型、数据与服务一体化管理。并针对我军建模与仿真应用领域不广、协作共享不够、数据与服务管理欠缺的问题,提出了相应的建议。     

DS/FH中窄带干扰的变换域处理方法研究

分别给出了DS/FH混合扩频系统中窄带干扰的两种变换域处理方法。具体分析了基于频域FFT和时频域M_PWD分析的被干扰谱线检测与抑制算法 ,为避免谱泄漏 ,在变换处理之前加窗处理。给出了不同处理算法情况下系统误码率的数字仿真结果     

塞式喷管高度特性的 CFD 研究

采用NND2M差分格式 ,从考虑k-ε湍流模型的理想气体三维薄层近似NS方程出发 ,对塞式喷管内外流场以及比冲随高度变化特性进行了数值研究 ,得到了较为准确的结果。计算表明 ,塞式喷管的低空性能明显优于传统喷管 ,NND2M差分格式及相应计算软件适合于模拟复杂喷流流场 ,可用于塞式喷管发动机的研究中。     

区域结构及多尺度纹理分析

结合纹理的结构分析方法 ,提出一种区域状结构 ,并把这种结构作为尺度空间中的特征。在基于区域状特征结构的尺度空间中 ,结构状纹理分析可转化为尺度空间中对特征结构的分析 ,从而实现了对纹理的多尺度分析。理论分析和实验结果证明了这种分析方法的有效性     

外光电效应中光电流的计算

根据金属中电子系统可假设为具有质量为m的粒子组成的理想费密气体,其在热平衡时服从费密-狄喇克分布规律,导出单位强度单色光束照射金属时所感生的光电流.     

多目标决策中基于遗传算法的方案排序分析

分析了常规多目标决策的一般过程,提出在进行方案排序综合时,应充分利用已得到的信息,据此建立了非线性规划模型,并引入遗传算法对规划模型进行求解.通过对实例进行分析,得出这种方法能充分利用集结后的信息,得到较为可信方案排序的结论.