分层海洋中求取本征声线数值方法研究

对分层海洋中本征声线的求取方法进行了改进.在本征声线模型基础上,分别利用二分法、单点弦截法对初始掠射角进行了精确计算和分析,结果表明,单点弦截法在保证精度的基础上节省了计算时间.计算结果可以为分层海洋本征声线建模提供理论依据.     

基于卷积神经网络的末敏弹复合探测信号识别方法北大核心CSCD

为了进一步提升末敏弹的目标识别性能,提出一种基于卷积神经网络(Convolutional Neural Network,CNN)的复合探测信号识别方法。首先针对毫米波辐射计、激光测距雷达和红外敏感器的复合探测信号特点,提出了3种构造输入样本的方法;然后根据不同的信息融合方式,提出了3种基本网络架构,分别构建了单通道、多通道CNN模型对输入信号进行特征提取和分类;最后通过高塔试验数据对模型进行训练和评估。测试结果表明,基于样本构造方案2和网络结构3的识别方法表现最佳,测试准确率达到了97.26%,所提样本构造方法和识别方法能够有效提取复合探测信号的特征,具有较高的识别精度。     

破甲杀伤复合战斗部仿真研究

研究EFP毁伤效能优化问题,为增加常规EFP战斗部对目标周围有生力量与轻型装甲目标的毁伤效能,通过在战斗部周向增填球形预制破片的方式,提出一种轴向EFP、周向预制破片的新型破甲杀伤复合战斗部结构.针对一种结构尺寸,在考虑粘合剂、冲击载荷下材料动态性能的变化、破片之间的相互作用等因素下进行了数值模拟研究,应用LS-DYNA软件分析了成型结果与破片场的杀伤能力,最后研究了药型罩壁厚、内衬尺寸以及破片直径对上述类型战斗部的成型与杀伤能力的影响规律,可以为战斗部的多功能毁伤设计提供帮助.     

应用Bayes方法进行末敏弹抛射过程可靠性分析

针对末敏弹是几种高新技术相结合的新型弹药．试验费用昂贵．靶场试验次数的特点．采用Bayes方法对其抛射过程的可靠性进行分析。详细分析了末敏弹的抛射过程．利用继承因子和环境因子对其各环节的验前信息进行了处理．并对抛射过程的可靠度进行了数值仿真计算．计算结果可以为下一步进行末敏弹的效能分析提供参考和依据。     

一种新型水下爆炸冲击等效加载实验方法

针对传统水下爆炸冲击响应实验研究中存在的问题,提出了一种实验室仿真水下爆炸冲击的等效加载方法,通过飞片撞击的方式来获得水下爆炸冲击等效载荷.同时建立了等效理论模型与流固耦合数值仿真来进行对比分析.结果表明,数值仿真结果与理论分析结果吻合较好,通过调节飞片的撞击速度与撞击比质量可以获得不同水下爆炸冲击所需要的等效载荷,进而为鱼雷爆炸对典型舰船结构的冲击响应研究提供一种新的思路.     

Computational and Experimental Investigation on Aerodynamic Characteristics of Terminally Sensitive Projectile with S-C Shaped Fins

The design of terminally sensitive projectile scanning platform requires a better understanding of its aerodynamic characteristics.The terminally sensitive projectile with S-C fins has a complex aerodynamic shape,which is constructed with small length to diameter ratio cylindrical body on which two low aspect ratio fins are installed.The study focuses on the effect of fin aspect ratio on the aerodynamic characteristics.Simulation was carried on based on computational fluid dynamics(CFD) method,and the pressure distribution characteristic,drag coefficient,lift coefficient and rolling moment coefficient varying with attack angle were obtained.A free flying experimental investigation focused on the kinetic aerodynamics was made.The results show that the fins provide sufficient drag to balance the terminally sensitive projectile weight to keep it flying at low and stable speed.The lift coefficient has a negative linear varying with attack angle.The rolling moment decrease with the increase in attack angle and the decrease in wing span area.     

Dynamic Study on Rigid and Flexible Coupling System for Terminally Sensitive Submunition

A kinetic model of the rigid and flexible coupling system for terminally sensitive submunition is set up with Kane＇s method. The parachute is considered as a flexible body, the flexible displacement is expressed with modal spread method, the position of the parachute is expressed with a hybrid coordinate method, and the kinematics of the terminally sensitive submunition is analyzed. Ten generalized coordinates relative to the attitude of the terminally sensitive submunition are chosen, and the correlative generalized active forces, the generalized inertial forces, the generalized internal forces are calculated in turn. On the base of the Kane＇s method, the ten degrees of freedom dynamic equations for the coupled terminally sensitive submunition are finally set up. This model can be used to expediently simulate and analyze accurately the exterior ballistic trajectory of terminally sensitive submunition, and provide the overall design of the terminally sensitive submunition with some helpful references.     

一种非对称双翼结构弹丸减速导旋特性试验研究

非对称双翼结构弹丸利用两个大小不同的刚性翼片提供非对称的气动力和气动力矩使弹丸形成所需的稳态扫描运动.为了分析非对称双翼结构弹丸的减速导旋特性,文中设计了一种非对称双翼结构弹丸的高塔投放试验方法,通过改变翼片形状、翼片面积及翼片布局,分析了不同非对称双翼结构对弹丸实现减速导旋性能的影响.     

新款啤酒鸭四例

笔者将啤酒用于鸭的烹调上,制作出了系列啤酒鸭授,深受客人好评,现介绍四款给大家,以供参考。一、鲜荷啤酒坛子鸭原料：家养鸭1只（约1500克）熟金华火腿60克腊鸡腿2个水发香菇50克猪街子骨回根鹌鹑蛋20个鲜荷叶2张香料30克冰箱40克糖色15克生姜、小葱各25克味精2克胡椒粉2克啤酒1600克色拉油100克精盐、麻油、酱油各适量①9．1、鸭宰杀洁净,斩成大小一致的方块：熟火腿切片;腊鸡腿用热水洗净,斩成6块;猪筒子骨捶断;鹤鹌蛋煮熟剥壳．用水漂去蛋表面的膜;生姜切片;小葱一部分打结．一部分切葱花;鲜荷叶洗净,用沸水稍烫。均待用…     

弹性翼S-C型末敏弹气动特性研究

采用双向流体-固体耦合方法对无伞末敏弹进行气动弹性分析,研究了末敏弹尾翼在气动力作用下的变形规律,并对尾翼变形后的末敏弹系统进行气动特性分析,总结了末敏弹气动参数、尾翼挠曲变形随运动攻角的变化规律。研究结果表明,末敏弹的阻力系数和转动力矩系数均随着攻角的增大呈先增加、后减小的趋势,升力系数则随着攻角的增大呈单调递增趋势;自由飞行试验结果显示,与刚性翼末敏弹相比,弹性翼末敏弹的气动参数仿真值与试验值更为贴近。