常用刺激剂及其分散技术

近几年来,无人机集群技术在美军多个方面的推动下,引起了全世界的热切关注。文章简要总结了美军无人机集群发展现状,梳理了美军开展无人机集群技术的初衷,并分析认为美军数量型无人机集群发展战略不完全适用于现阶段我军军情。文中给出了我国现阶段发展无人机集群的思路,这对全面认识无人机集群的优势、明晰我军无人机集群技术发展方向具有一定的参考价值。     

环肋圆柱壳模型在水下爆炸响应试验中的边界条件

为验证试验研究中环肋圆柱壳模型的边界条件,运用大型商业有限元程序MSC.DYTRAN分别设置3种边界条件,对试验过程进行了数值仿真研究。壳体塑性变形的仿真过程显示,迎爆面中部首先变形,随后侧爆面和背爆面相继变形,壳体最终形成数个凸凹相间的轴向凹凸带,最大塑性变形发生在迎爆面中心肋位。壳体塑性变形的仿真计算结果与试验结果的对比结果表明:固支边界条件符合试验实际情况。该结论适用于试验研究中模型边界条件的确立。     

油库储油区燃烧爆炸事故树分析

针对油库储油区安全管理点多面广的特点,分析储油区燃烧爆炸事故的相关影响因素和条件,建立完善的事故树模型。通过定性分析理清燃烧爆炸事故与基本事件之间的逻辑关系,定量分析获得各项基本事件的结构重要度排序,找出储油区存在燃烧爆炸隐患的重点部位,制订科学合理的安全信息监控点设置策略,为油库安全管理手段向信息化迈进提供决策依据。     

对称螺杆流量计转子热变形的综合分析

利用有限元理论对８０ｍｍ口径的对称螺杆流量计转子的热变形进行了综合分析．整个计算程序分为平衡和非平衡两套系统．通过计算转子的热变形,推导出热变形对转子泄漏和运转等方面的影响．最后得出对生产有指导意义的具体数值和具体方法．     

舰船单元结构模型水下接触爆炸破口试验研究

以 3种舰船单元结构模型水下接触爆炸试验为基础 ,对结构模型所产生的变形、破口尺寸、破口形状进行了观测与分析 ,查找并发现结构中的薄弱环节 .提出了板架结构加强筋相对刚度概念 ,确定了破口长度的估算系数 ,同时为舰船结构在水下爆炸作用下的破口数值计算提供了试验数据 ,如材料断裂极限应变等     

舰船电缆热老化寿命的研究

介绍了某船用电缆热老化寿命研究的有关试验和结果分析．对电统绝缘材料失效的判断、机械性能变化的预测,以及如何根据电缆的负载情况和周围的环境温度确定绝缘材料的老化温度等,提出了相应的观点和方法．     

Mechanical properties and thermal conductivity of pristine andfunctionalized carbon nanotube reinforced metallic glass composites:A molecular dynamics approach

This work uses the molecular dynamics approach to study the effects of functionalization of carbon nanotubes (CNTs) on the mechanical properties of Cu64Zr36 metallic glass (MG). Three types of functional groups, carboxylic, vinyl and ester were used. The effect of CNT volume fraction (Vf) and the number of functional groups attached to CNT, on the mechanical properties and thermal conductivity of CNT-MG composites was analysed using Biovia Materials Studio. At lower values of Vf (from 0 to 5％), the per-centage increase in Young's modulus was approximately 66％. As the value of Vf was increased further (from 5 to 12％), the rate of increase in Young's modulus was reduced to 16％. The thermal conductivity was found to increase from 1.52 W/mK at Vf=0％to 5.88 W/mK at Vf=12％, thus giving an increase of approximately 286％. Functionalization of SWCNT reduced the thermal conductivity of the SWCNT-MG composites.     

Effect of organo-modified montmorillonite nanoclay on mechanical,thermal and ablation behavior of carbon fiber/phenolic resin composites

The mechanical, thermal and ablation properties of carbon phenolic (C-Ph) composites (Type-I) rein-forced with different weight percentages of organo-modified montmorillonite (o-MMT) nanoclay have been studied experimentally. Ball milling was used to disperse different weight (wt) percentages (0, 1,2,4,6 wt.％) of nanoclay into phenolic resin. Viscosity changes to resin due to nanoclay was studied. On the other hand, nanoclay added phenolic matrix composites (Type-II) were prepared to study the dispersion of nanoclay in phenolic matrix by small angle X-ray scattering and thermal stability changes to the matrix by thermogravimetric analyser (TGA). This data was used to understand the mechanical, thermal and ablation properties of Type-I composites. Inter laminar shear strength (ILSS), flexural strength and flexural modulus of Type I composites increased by about 29％, 12％and 7％respectively at 2 wt.％ addition of nanoclay beyond which these properties decreased. This was attributed to reduced fiber volume fraction (％Vf) of Type-I composites due to nanoclay addition at such high loadings. Mass ablation rate of Type-I composites was evaluated using oxy acetylene torch test at low heat flux (125 W/cm2) and high heat flux levels (500 W/cm2). Mass ablation rates have increased at both flux levels marginally up to 2 wt.％ addition of nanoclay beyond which it has increased significantly. This is in contrast to increased thermal stability observed for Type-I and Type-Ⅱ composites up to 2 wt.％addition of nanoclay. Increased ablation rates due to nanoclay addition was attributed to higher insulation effi-ciency of nanolcay, which accumulates more heat energy in limited area behind the ablation front and self-propagating ablation mechanisms triggered by thermal decomposition of organic part of nanoclay.     

Improvement of VIS and IR camouflage properties by impregnating cotton fabric with PVB/IF-WS2

In order to examine the possibility to improve its camouflage properties standard cotton fabric with camouflage print was impregnated with poly(vinyl butyral), PVB and fullerene-like nanoparticles of tungsten disulfide, PVB/IF-WS₂. FTIR analysis excluded any possible chemical interaction of IF-WS₂ with PVB and the fabric. The camouflage behavior of the impregnated fabric has been examined firstly in the VIS part of the spectrum. Diffuse reflection, specular gloss and color coordinates were measured for three different shades (black, brown and dark green). Thermal imaging was applied to examine the camouflage abilities of this impregnation in IR part of the spectrum. The obtained results show that PVB/IF-WS₂ impregnation system induced enhacement of the materials camouflage properties, i.e. that IF-WS₂ have a positive effect on spectrophotometric characteristics of the fabric.     

An interface shear damage model of chromium coating/steel substrate under thermal erosion load

The Cr-plated coating inside a gun barrel can effectively improve the barrel's erosion resistance and thus increase the service life.However,due to the cyclic thermal load caused by high-temperature gun-powder,micro-element damage tends to occur within the Cr coating/steel substrate interface,leading to a gradual deterioration in macro-mechanical properties for the material in the related region.In order to mimic this cyclic thermal load and,thereby,study the thermal erosion behavior of the Cr coating on the barrel's inner wall,a laser emitter is utilized in the current study.With the help of in-situ tensile test and finite element simulation results,a shear stress distribution law of the Cr coating/steel substrate and a change law of the interface ultimate shear strength are identified.Studies have shown that the Cr coating/steel substrate interface's ultimate shear strength has a significant weakening effect due to increasing temperature.In this study,the interfacial ultimate shear strength decreases from 2.57 GPa(no erosion)to 1.02 GPa(laser power is 160 W).The data from this experiment is employed to establish a Cr coating/steel substrate interface shear damage model.And this model is used to predict the flaking process of Cr coating by finite element method.The simulation results show that the increase of coating crack spacing and coating thickness will increase the service life of gun barrel.