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381.
《防务技术》2020,16(3):678-688
Multilayer materials are widely used in military, automobile and aerospace industries. In this paper, the response of an explosion-welded Ti6Al4V/pure titanium with a flat interface to dynamic loading is investigated. An SHPB apparatus is used. Then, the dynamic behaviour of a bimetal sample is explored with a DIC system coupled to the SHPB. Result indicates that in the bimetal sample pure titanium is deformed and failed before Ti6Al4V. The stress curve of the sample shows two different peaks in a striker velocity higher than the 18.3 m/s. When the incident wave encounters the interface of the Ti6Al4V/pure titanium sample, only a small fraction of the wave is reflected owing to similar impedance. Using the direct interpretation stress-strain curve is unreasonable in this case because of unhomogenised plastic deformation. The microstructure of the sample is investigated after loading. An adiabatic shear band is formed in the pure titanium side before failure, and the interface of the sample remains intact under different loading conditions. The FEM simulation result for the sample is in good agreement with experimental observations.  相似文献   
382.
《防务技术》2020,16(6):1167-1187
The load-carrying capacities and failure patterns of reinforced concrete components can be significantly changed by membrane effects. However, limited work has been carried out to investigate the blast resistance of Hybrid Fiber Reinforced Lightweight Aggregate Concrete (HFR-LWC) members accompanying membrane action. This paper presents a theoretical approach to quantitatively depicting the membrane behavior and its contribution on the behavior of HFR-LWC beams under close-range blast loadings, and the suitability of the proposed model is validated by a series of field tests. An improved Single-Degree-of-Freedom (SDOF) model was employed to describe the dynamic responses of beam-like members under blast loadings accompanying membrane action, where the mass-load coefficient is determined according to the nonuniformly distributed load induced by close-range explosion, and the membrane action is characterized by an in-plane (longitudinal) force and a resisting moment. The elasto-plastic and recovery responses of HFR-LWC beams under the combined action of blast load and membrane force were analyzed by the promoted model. A specially built end-constrain clamp was developed to provide membrane action for the beam member when they are subjected to blast load simultaneously. It is demonstrated that the analytical displacement-time histories are in good agreement with experimental results before peak deflections and that the improved SDOF model is an acceptable tool for predicting the behavior of HFR-LWC beams under blast loadings accompanying membrane action.  相似文献   
383.
介绍了产品数据管理(PDM)的概念和基本功能,结合当前型号研制的特点和计算机信息技术应用的状况、发展,研究了型号研制产品数据管理的需求、功能及实施,为当前型号研制依靠CIMS技术实现产品数据管理提出了8条基本原则。  相似文献   
384.
Groebner基下分离子插值函数模型   总被引:1,自引:0,他引:1  
给出Groebner基下建立分离子插值函数模型的方法。对于任意离散时间序列可在字典序下找到相关分离子,并用此分离子构建该离散时间序列的函数模型,及其满足所给点列的多元插值函数。通过实例说明了模型建立过程。  相似文献   
385.
Using annual data collected from 1988 to 2015, this study provides evidence of a non-linear relationship between military spending, economic growth and other growth determinants for the South African economy. The empirical study is based on estimates of a logistic smooth transition regression (LSTR) model and our empirical results point to an inverted U-shaped relationship between military spending and economic growth for the data. Furthermore, our empirical results suggest that the current levels of military spending, as a component of total government expenditure, are too high in the South African economy and need to be transferred towards more productive non-military expenditure in order to improve the performance of economic growth and other growth determinants.  相似文献   
386.
在现有的RFID标准中,一般标签ID都由几个不同含义区间组成。针对这种特点,提出推断式二进制防碰撞算法:在识别每个区间段的ID时,利用某个特定读写器中的前缀库推断该区间段各个位的取值,以便减少待识别标签ID的位数。同时,通过调整参数u,可以对系统可靠性进行控制。仿真实验表明,在没有新前缀出现的情况下,推断式二进制防碰撞算法能够将QT算法的识别速度提高3倍、标签平均响应次数降低3/4。  相似文献   
387.
应用于飞行器隐身等离子体的分析   总被引:2,自引:0,他引:2  
根据雷达波隐身对等离子体电子数密度的要求 ,分析计算说明了热平衡与非热平衡等离子体以及冷等离子体可应用于飞行器的隐身。通过对等离子体不同产生方法、临界电子数密度的分析以及气体击穿电场强度的计算 ,归结出了不同等离子体的特点 ,并进而说明用稳态电源以及微波源产生的等离子体适合应用于飞行器隐身  相似文献   
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