Interactions of Impact Shock Waves in a Thin-Walled Explosive Container. II. Impact by a Cone-Nosed Projectile

Interaction of impact shock waves that could detonate an explosive (Composition B) confined in a thin-walled container impacted by a cone-nosed projectile is numerically studied, based on the Forest Fire explosive reaction rate model. The normal impact on the container by a small projectile with a conical nose is considered. Depending on the cone angle of the nose part of the projectile, the zone of interaction of initiating shock waves can be remote from the central axis of the impact. The off-the-central-axis detonation is interpreted from the viewpoint of different interaction modes in the explosive container, which are reflected from the cassette wall, change their directions, and superimpose onto each other, leading to explosive detonation.     

小波包变换在火箭发动机脉动压力分析中的应用

在火箭发动机试验中,燃烧室脉动压力数据是考察推进剂燃烧状态的重要依据.通过对脉动压力数据特征分析,利用小波包变换多分辨分析的特点,以信噪比作为衡量标准,采用小波包自选阈值法对脉动压力数据进行去噪.通过与稳态参数数据的对比验证了去噪结果的准确性.采用Wicherhauser树状分解和Shannon信息熵基波选择标准等方法对脉动压力数据进行分频段分析.根据结果中各频段内的系数特征能够直观分析脉动压力在各频带中的能量分布.通过对脉动压力数据和相应振动测点数据的频谱分析,验证了分析结果的有效性.该方法在其他型号发动机和组合件试验脉动压力数据分析中有重要的应用和推广价值.     

Sealing of Ejection Hole at the Bottom of Projectile for Wired Transmission System of Penetration Data

It is difficult to find the projectile when people want to get the penetration data in a hard recovery method, so a recovery system of penetration data is designed based on an ejection mode from the projectile base and a method of wired transmission, at the same time, the system was sealed with a designed sealing device, the working principle of which was introduced. Using Fluent as the simulation platform, the transient pressure of seal cavity was simulated based on the change of chamber pressure, and steady-state pressure of seal clearance and seal cavity were simulated based on the maximum chamber pressure. The sealing performance was tested by a pressure test system. The results of simulation and experiment show that the maximum pressure of seal cavity is 139.4.kPa when the maximum chamber pressure is 242.9.MPa and the maximum temperature of gunpowder explosive gas is 2.166.5.K, so the sealing performance can be assured. The sealing device can be taken as a reference in sealing research on gunpowder gas at the bottom of projection.     

不同头型高速射弹垂直入水数值模拟

为研究不同射弹头型对高速射弹垂直入水的流体动力和流场特性的影响,采用有限体积法和VOF(volume of fluid)多相流模型,并引入动网格技术,对5种不同头型的轴对称高速射弹垂直入水过程进行了数值模拟,分析了头型对空泡形态演化过程、射弹流体动力及弹道特性的影响规律.研究结果表明,头型对射弹入水空泡形态、表面闭合时间以及入水阻力、深度、速度均有较大影响.球头与截球头空泡半径小于其余3种头型,表面闭合时刻依平头、球头、锥头、截锥头的顺序递增.射弹头部均承受较大压力,球头、截球头射弹头部压力分布不均使之承受较大的剪切力.射弹头部流线型越好,入水速度衰减越慢,入水深度增加越快.入水阻力系数峰值按平头、截球头、截锥头、锥头、球头的顺序递减.     

Q235钢板对平头弹抗侵彻特性研究

为分析靶体结构对其抗侵彻特性的影响,利用轻气炮进行平头杆弹正撞击单层板和等厚接触式三层板的实验,获取相关的撞击过程图片.通过撞击实验,得到这两种结构靶体的初始-剩余速度曲线以及弹道极限,撞击速度为190~450 m/s.研究靶体结构对抗侵彻特性的影响,包括靶板的失效模式和抗侵彻性能.最后,采用ABAQUS/EXPLICIT软件对杆弹撞击金属板的过程进行数值模拟研究,通过对比数值模拟和实验结果,验证了数值模拟材料模型和参数的有效性.结果表明:多层板的弹道极限高于等厚单层板,并且多层板和单层板的主要失效模式之间存在差异.对于多层板,靶板失效模式与其在靶中位置相关.     

旋转弹攻角测试的特征值神经网络算法

对应用于旋转弹攻角测试的嵌入式大气数据传感(FADS)算法进行了分析.经加噪数据仿真检验,表明FADS算法解算得到的攻角误差与压力误差为线性关系;以空气动力学模型为基础,使用压力数据构建了具有非时变稳定性的两个特征值,仅与攻角、马赫数有关;选取不同攻角、马赫数组合状态下的特征值作为神经网络的训练样本,应用同样的加噪数据仿真检验,表明基于特征值的神经网络算法的抗干扰特性优于FADS算法;用风洞试验数据进行攻角解算,表明神经网络算法得到的攻角没有跳变现象,比FADS算法误差更小,具有更好的抗干扰性.     

易碎弹复合材料动态特性数值研究

利用Split Hopkinson Pressure Bar （SHPB）实验装置获取复合材料易碎弹试件的动态力学特性,并应用LS-DYNA软件对SHPB实验过程进行数值模拟.结合SHPB应力波理论,研究不同撞击速度对试件破坏程度、压杆轴向应变波形以及试件动态力学特性的影响.仿真结果表明：试件仿真结果与实验结果基本吻合,说明SHPB实验仿真是可行的;试件的破坏程度随着撞击速度的增大而显著,但压杆轴向应变波形以及试件动态力学特性随着撞击速度的增大变化不明显.     

Liquid Impact Based Material Micro-Forming Technology

The objective of this study was to investigate material deformation in the course of a high-speed (>1500 m/s) water impact and to use the acquired knowledge for improvement of the forming technology. An experimental setup for projectile fabrication was constructed and a series of experiments involving sub-millimeter and micron scale metal deformation was performed. The geometry and topography of the generated samples were investigated using advanced surface examination techniques and the feasibility of the liquid impact based micro-forming technology was demonstrated. This article was presented at Materials Science & Technology 2006, Innovations in Metal Forming symposium held in Cincinnati, OH, October 15-19, 2006.     

发动机初级工况对冷却夹套隔片损伤影响分析

针对可重复使用液体火箭发动机推力室冷却夹套隔片的损伤问题,为确保发动机的工作寿命,对建立了冷却夹套隔片的夹芯梁结构模型、粘塑性模型和细化损伤模型,发动机起动过程中初级工况给冷却夹套隔片损伤发展的影响进行了仿真计算。结果表明:初级工况过高,压力等性能参数振荡明显,振幅也较大,但引起的冷却夹套隔片损伤较小;初级工况选择过低,引起的冷却夹套隔片损伤较大,且压力等性能参数振荡也比较明显,但振幅较小。通过对比分析给出了用于发动机起动的合适初级工况,采用此工况使发动机起动过程中引起的损伤较小,而且压力等性能参数的振荡也较小。     

湿度和温度对聚合物光纤光栅反射波长漂移量的影响

针对固体火箭发动机纤维缠绕壳体状态监测中局部可能出现大应变情况,采用聚合物光纤布拉格光栅(polymer op-tical fiber Bragg grating,POFt3G)传感器对大应变进行检测;分析了湿度和温度对光纤光栅反射波长漂移量的影响,建立了湿度传感模型、温度传感模型和温度湿度混合模型.并通过MATLAB进行数值仿真,结果表明,反射波长随温度的升高而减小,随湿度的增加而增大,并受到温度和湿度的交叉影响,这与文献报道的实验结果比较吻合.