火控系统总体设计综合技术

本文对火控系统总体设计综合技术中的一些重要问题,如指标体系,系统效能、总体方案的制定及翩定方案的准则进行了分析讨论,提出了一些看法,问题和建议.     

21世纪无人机关键技术

无人机因其独特而优异的战术性能,在近几次现代局部战争中得到了越来越广泛的应用,执行的任务也越来越多。从未来无人机的军事需求及其战术性能入手,结合技术发展趋势和发展可行性,对未来无人机发展需要的一些关键技术进行了分析研究,这些关键技术对提高未来无人机的战术性能具有重要作用。     

推进剂利用系统装订参数计算及软件集成方法

在大型航天软件中,推进剂利用系统装订参数计算对提高推进剂利用率具有重要意义。给出了利用系统装订参数的计算方法,并在基于CORBA的分布式大型软件系统中对软件集成方法进行了研究。     

火炮装药温度分布的数值模拟

针对火炮弹药的特点,建立了弹药的二维轴对称模型,并在圆柱坐标系下,用控制容积积分法导出一组差分离散格式。采用收敛速度快的块迭代法解代数方程组。实验数据表明数值计算的结果和实测值基本一致,经进一步研究可以用于火炮装药的温度测量。     

基于ANSYS的预应力CFRP布加固混凝土梁有限元分析

采用ANSYS有限元分析软件,对卸载或不卸载时预应力碳纤维(CFRP)布加固梁进行仿真分析,并在有限元分析中提出了施加预应力的方法(升温法),以及利用单元的生与死实现不卸载时加固的方法。通过实例对比分析表明,基于ANSYS的有限元分析结果与试验分析结果吻合较好,可在一定程度上有效替代试验分析方法,从而减少试验所需的时间和费用,对后续的CFRP布加固混凝土结构的研究工作具有一定的参考价值。     

末端防御武器系统的人机一体化

如何实现人在末端防御武器系统运行中所应该起的作用,并为实现这些作用提供必需的保障,对末端防御武器系统的研制、试验和使用至关重要。要做到这一点,应该通过自顶向下的人机一体化的需求分析,确定人在系统中所应完成的作用并且明确为完成此作用而对系统提出的要求。系统的设计应该遵循人机一体化的原则,提高系统的自动化程度,减少人的工作负荷,减少人员配备。系统要保障人为完成其作用而所需的条件,向人提供有关完成其作用所必需的知识,使人在执行其所担负的任务中不出差错。     

海战场信息系统和武器系统综合仿真技术研究

本文分析了海战场信息系统仿真的特点,介绍了可以应用于海战场信息系统和武器系统综合仿真的高层体系结构(HLA)技术,描述了澳大利亚国防科学与技术组织(DSTO)基于HLA技术的虚拟舰艇概念和潜在的应用,以及虚拟舰艇结构和层次化联邦共同体概念的设计方法。     

Optimization of buckling load for laminated composite plates using adaptive Kriging-improved PSO: A novel hybrid intelligent method

An effective hybrid optimization method is proposed by integrating an adaptive Kriging (A-Kriging) into an improved partial swarm optimization algorithm (IPSO) to give a so-called A-Kriging-IPSO for maxi-mizing the buckling load of laminated composite plates (LCPs) under uniaxial and biaxial compressions. In this method, a novel iterative adaptive Kriging model, which is structured using two training sample sets as active and adaptive points, is utilized to directly predict the buckling load of the LCPs and to improve the efficiency of the optimization process. The active points are selected from the initial data set while the adaptive points are generated using the radial random-based convex samples. The cell-based smoothed discrete shear gap method (CS-DSG3) is employed to analyze the buckling behavior of the LCPs to provide the response of adaptive and input data sets. The buckling load of the LCPs is maximized by utilizing the IPSO algorithm. To demonstrate the efficiency and accuracy of the proposed methodology, the LCPs with different layers (2, 3, 4, and 10 layers), boundary conditions, aspect ratios and load patterns (biaxial and uniaxial loads) are investigated. The results obtained by proposed method are in good agreement with the literature results, but with less computational burden. By applying adaptive radial Kriging model, the accurate optimal results-based predictions of the buckling load are obtained for the studied LCPs.     

Bionic stab-resistant body armor based on triangular pyramid structure

A stab-resistant substrate was designed and realized with a triangular pyramidal structure, inspired by the biological armor model in nature. The stab-resistance behavior and dynamic response mechanisms were studied through numerical simulation and experimental testing of a knife impacting a substrate, and an optimal structural design was obtained accordingly, with a tilted angle of 22.5° and optimal thickness of 1.2 mm. It was shown that the triangular pyramidal structure generated twice the internal energy of the knife than the flat substrate due to the dispersing effect of the structure. The force parallel to the inclination caused a significant scratch on the substrate surface, while the force perpendicular caused obvious substrate deformation. A new riveting method was used to form the total layer, which passed the GA 68—2008 standard. The stab-resistant clothing coupled with the reduced wearing burden could provide effective protection and avoid fatal injuries on security personnel working in dangerous environments. The method provided may enlighten the future design and manufacturing of stab-resistant clothing.     

Dynamic necking of a near α titanium alloy at high strain rates:Experiments and modelling

The tensile behaviour of near α Ti3Al2.5 V alloy, conceived for applications in aerospace and automotive engineering, is characterized from quasi-static to high strain rates. The material is found to present noticeable strain rate sensitivity. The dynamic true strain rate in the necking cross-section reaches values up to ten times higher than the nominal strain rate. It is also observed that beyond necking the dynamic true stress-strain curves present limited rate dependence. The experimental results at different strain rates are used to determine a suitable constitutive model for finite element simulations of the dynamic tensile tests. The model predicts the experimentally macroscopic force-time response, true stress-strain response and effective strain rate evolution with good agreement.