基于SLPP-LSSVM的空战效能评估研究

针对现代空战效能评估多层次、多因素、非线性耦合的复杂特点,提出一种基于有监督局部保留投影(SLPP)和最小二乘支持向量机(LSSVM)的空战效能综合评估模型.先利用SLPP对数据局部信息和类别信息的处理能力,提取空战效能数据中有辨识力的低维特征;利用获取的低维特征构建LSSVM空战效能综合评估模型;通过构建的模型,对空战效能进行评估.计算分析表明,所提出模型的评估结果与专家的评估结果相一致,没有出现错判,不同参数下结果输出也很稳定.因此,将该模型用于空战效能评估是有效和可行的,也为空战效能评估提供了一种可靠的技术途径.     

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.     

Fracture mechanism of a cylindrical shell cut by circumferential detonation collision

The failure mechanism of a cylindrical shell cut into fragments by circumferential detonation collision was experimentally and numerically investigated. A self-designed detonation wave regulator was used to control the detonation and cut the shell. It was found that the self-designed regulator controlled the fragment shape. The macrostructure and micro-characteristics of fragments revealed that shear fracture was a prior mechanism, the shell fractured not only at the position of detonation collision, but the crack also penetrated the shell at the first contact position of the Chapmen-Jouguet (C-J) wave. The effects of groove number and outer layer thickness on the fracture behavior were tested by simulations. When the thickness of the outer layer was 5–18 mm, it has little effect on fragmentation of the shell, and shells all fractured at similar positions. The increase of the groove number reduced the fracture possibility of the first contact position of the C-J wave. When the groove number reached 7 with a 10 mm outer layer (1/4 model), the fracture only occurred at the position of detonation collision and the fragment width rebounded.     

An experiment evaluating how the tiny mass eccentricities in spin-stabilized projectiles affect the position of impact points

This study investigates and quantifies some possible sources affecting the position of impact points of small caliber spin-stabilized projectiles (such as 12.7 mm bullets). A comparative experiment utilizing the control variable method was designed to figure out the influence of tiny eccentric centroids on the projectiles. The study critically analyzes data obtained from characteristic parameter measurements and precision trials. It also combines Sobol's algorithm with an artificial intelligence algorithm—Adaptive Neuro-Fuzzy Inference Systems (ANFIS)—in order to conduct global sensitivity analysis and determine which parameters were most influential. The results indicate that the impact points of projectiles with an entry angle of 0° deflected to the left to that of projectiles with an entry angle of 90°. The difference of the mean coordinates of impact points was about 12.61 cm at a target range of 200 m. Variance analysis indicated that the entry angle — i.e. the initial position of mass eccentricity — had a notable influence. After global sensitivity analysis, the significance of the effect of mass eccentricity was confirmed again and the most influential factors were determined to be the axial moment and transverse moment of inertia (Izz Iyy), the mass of a projectile (m), the distance between nose and center of mass along the symmetry axis for a projectile (Lm), and the eccentric distance of the centroid (Lr). The results imply that the control scheme by means of modifying mass center (moving mass or mass eccentricity) is promising for designing small-caliber spin-stabilized projectiles.     

Mitigation effects on the reflected overpressure of blast shock with water surrounding an explosive in a confined space

The mitigation of blast shock with water has broad application prospects. Understanding the mitigation effects on the reflected overpressure of the explosion shock with water surrounding an explosive in a confined space is of great significance for military explosives safety applications. To estimate the effects of the parameters on the reflected overpressure of blasted shock wave, a series of experiments were carried out in confined containers with spherical explosives immersed in a certain thickness of water, and numerical simulations were conducted to explore the corresponding mechanisms. The results reveal that the reflected overpressure is abnormally aggravated at a small scaled distance. This aggravation is due to the high impulse of the bulk accelerated water shell converted from the explosion. With increasing scaled distance, the energy will be gradually dissipated. The mitigation effects will appear with the dispersed water phase front impacting at a larger scaled distance, except in the case of a dense water phase state. A critical scaled distance range of 0.7—0.8 m/kg1/3 for effective mitigation was found. It is suggested that the scaled distance of space walls should be larger than the critical value for a certain water-to-explosive weight ratio range (5—20).     

以太网交换机仿真与验证

叙述了以太网交换机的结构、端口缓存交换策略,从排队论出发建立仿真模型和仿真流程,按数理统计原理用t函数进行均值假设检验,验证仿真模型及流程的可信度。文章叙述以太网交换机仿真模型与算法对进行计算机网络仿真有参考价值。     

通用油料装备质量分级研究

通用油料装备的质量分级是依据油料装备的不同技术状况划分质量等级,以便于装备的使用、维护、退役和报废。介绍了通用油料装备的质量分级应遵循的原则和质量等级划分的主要依据,将通用油料装备质量等级分为四等六级,每一级对应一个级值,给出了质量分级的数学模型,并提出了分级依据对应级值的条件或计算方法。     

装备维修管理系统的建立与运作

船艇装备维修管理系统是一种新型维修管理模式的总称,它不仅全面管理船艇装备的维修工作,也为这项工作的实施提供了技术指导．文章主要探讨系统建立及运作过程中的主要工作及方法,为这一系统在船艇装备上的应用奠定了基础．     

受压带肋圆柱壳体固有振动频率和稳定性计算

论述了丧失舱段总稳定性是潜艇耐压壳体在深潜时的主要破坏模式 .并将振动屈曲理论应用于潜艇耐压壳体稳定性的研究 ,在 Donell公式的基础上 ,导出了带肋圆柱壳体的整体固有振动频率与壳体所受外界水压之间的关系表达式 ,据此解出带肋圆柱壳体整体失稳的理论压力值 .最后 ,将公式的计算结果、实验结果和有限元法的计算结果进行比较 ,得出几点结论 .     

依托EDA平台,加速电工电子类课程教学改革

论述了在电工电子类课程中开展EDA教学的目的、意义和必要性,介绍了在现代化教学中进行EDA教学的经验、体会和成果,提出了进一步优化课程体系、加速电工电子类课程教学改革的思路和想法.