排水型方尾船加装尾板前后振动性能分析

采用大型通用有限元分析软件和流体边界元方法,对某排水型方尾船加装尾板前后的总体振动特性和尾部振动响应进行了分析计算和比较,得出了加装尾板对该型船总体振动特性和尾部振动响应影响很小的结论.     

含水乙醇燃烧的对冲扩散火焰数值研究

为加深对低浓度乙醇燃气发生器燃烧过程化学动力学过程的理解,分析水组分在燃烧过程中所起的作用,利用对冲扩散火焰模型对不同浓度下的火焰结构进行了数值分析,并虚拟了一种惰性水组分以区分物理机制和化学机制对燃烧过程产生的影响.研究结果显示,随着乙醇浓度的不断降低,火焰锋面呈现出向燃料侧的整体移动趋势;随着浓度向极限浓度的趋近,...     

基于振动分析的坦克柴油机汽缸燃烧压力检测方法

针对在坦克实车上不易直接测量柴油机汽缸压力的问题,提出了一种通过测量柴油机汽缸盖振动信号来间接检测汽缸燃烧压力的方法。在某型坦克柴油机上同步测量了汽缸燃烧压力、汽缸盖振动信号和变速箱振动信号,利用自适应滤波方法滤除了汽缸盖振动信号中包含的变速箱振动信号形成的噪声干扰,利用配气相位从时间域分离出由气体燃烧压力激发的振动信号,利用Hilbert变换和小波分解方法分别提取了振动信号和压力信号的特征波形。建立了RBF神经网络模型,以汽缸盖振动信号的包络作为网络输入,实现了汽缸燃烧压力的间接检测。     

数值模拟气液针栓式火箭发动机喷雾燃烧对声学激励的响应

为研究气液针栓式火箭发动机的声学振荡特性并为其优化设计提供指导,加工了具有矩形燃烧室的LOX/GCH₄针栓式发动机,采用Euler-Lagrange方法仿真横向速度扰动产生的声学响应,以期在热试前了解声学激励频率对非稳态喷雾燃烧过程的影响。仿真结果表明,采用的横向速度扰动能在燃烧室内产生同频率的一阶横向声学振荡响应。喷雾燃烧对声学激励的响应强弱受扰动频率与燃烧室一阶横向振荡模态固有频率的相对大小影响较大。当扰动频率与该固有频率相等时,压力和燃烧释热随速度扰动出现同相振荡,压力振荡幅值显著增高导致燃烧室前半段的喷雾和火焰同步摆动;同时,燃烧室内存在扩散燃烧变为预混燃烧的趋势,甲烷在更短的距离内燃烧完全且燃烧室温度趋于均匀。     

Recent advances in catalytic combustion of AP-based composite solid propellants

Composite solid propellants (CSPs) have widely been used as main energy source for propelling the rockets in both space and military applications. Internal ballistic parameters of rockets like characteristic exhaust velocity, specific impulse, thrust, burning rate etc., are measured to assess and control the performance of rocket motors. The burn rate of solid propellants has been considered as most vital parameter for design of solid rocket motors to meet specific mission requirements. The burning rate of solid propellants can be tailored by using different constituents, extent of oxidizer loading and its particle size and more commonly by incorporating suitable combustion catalysts. Various metal oxides (MOs), complexes, metal powders and metal alloys have shown positive catalytic behaviour during the com-bustion of CSPs. These are usually solid-state catalysts that play multiple roles in combustion of CSPs such as reduction in activation energy, enhancement of rate of reaction, modification of sequences in reaction-phase, influence on condensed-phase combustion and participation in combustion process in gas-phase reactions. The application of nanoscale catalysts in CSPs has increased considerably in recent past due to their superior catalytic properties as compared to their bulk-sized counterparts. A large surface-to-volume ratio and quantum size effect of nanocatalysts are considered to be plausible reasons for improving the combustion characteristics of propellants. Several efforts have been made to produce nanoscale combustion catalysts for advanced propellant formulations to improve their energetics. The work done so far is largely scattered. In this review, an effort has been made to introduce various combustion catalysts having at least a metallic entity. Recent developments of nanoscale combustion catalysts with their specific merits are discussed. The combustion chemistry of a typical CSP is briefly discussed for providing a better understanding on role of combustion catalysts in burning rate enhancement. Available information on different types of combustion nanocatalysts is also presented with critical comments.     

5－乙酰基－2－氨基二苯甲酮的合成

用对硝基苯乙酮、乙二醇、苯乙腈、氢气、高氯酸为原料,经酮基保护,环化,催化加氢和消除反应,合成出较高产率的5-乙酰基-2-氨基二苯甲酮。对反应机理作了初步探讨,并用元素分析、IR和1HNMR对其结构进行了表征。     

聚(2-甲氧基-5-丁氧基)亚苯基亚乙烯的合成及电性能

本文用对甲氧基苯酚、正溴丁烷、聚甲醛为原料， 经醚化， 双氯甲基化和碱性消除反应， 合成出长链共轭且可溶的聚（２甲氧基５丁氧基）亚苯基亚乙烯，用 Ｉ Ｒ 和１ Ｈ Ｎ Ｍ Ｒ 表征了中间体和聚合物的结构，并测定了聚合物的伏—安特性曲线。     

基于多特征模糊融合的疲劳状态判决

在基于视觉的疲劳驾驶识别过程中,使用单个特征进行疲劳驾驶判断,常常会受到非普遍适用性、噪声等因素的影响,从而导致识别率降低。为了解决眼部特征参数或者是嘴巴特征参数单个特征识别率低甚至特使环境无法识别的问题,提出一种基于多特征融合的判决方法,利用了各种特征之间的优势互补,可以降低噪声和类内类间差异的影响,从而提高系统的性能,并且能增强适用性。最后通过实验结果证明,使用眼部和嘴巴特征融合的方法比单一的判决方法准确率更高。     

滚动轴承故障诊断中的并行组合模拟退火算法研究

提出了一种基于并行组合模拟退火算法的故障识别新方法 ,详细讨论了该混合算法的原理及实现方法 ,并应用于滚动轴承早期故障诊断实例中 ,获得了好的结果 .     

鱼雷雷体特性对其惯性深控系统阶跃响应的影响

分析、对比了两种鱼雷雷体特性对惯性深控系统阶跃响应的影响 ,从中找出对鱼雷定深航行稳定性有较大影响的雷体参数 ,可以为鱼雷总体优化设计提供一定的参考