弹托前端结构对脱壳性能的影响

该文用四种弹托前端结构的25 mm APFSDS弹,在中间弹道靶道中进行了射击试验,利用正交多站火花阴影照相系统,得到了不同弹托脱壳过程的时序阴影照片.对照片的定量分析表明,弹托前端结构对弹托脱壳性能及弹体扰动有重要影响.     

穿甲威力试验方法的改进

引入单发临界穿透速度的概念，２数字仿真技术模拟穿甲威力试验结果，对出的试验结果进行分析，通过分析发现目前试验方法中的缺陷。并提出了改进的试验方法，与目前试验方法比较，改进的方法有很大的优越性。     

底部排气弹射程标准化方法初探

讨论了底排弹射程标准化方法所满足的要求，分析了现行底排弹射程标准化方法存在的问题，对底排减阻模型进行了改进，并对试验数据进行了分析处理。     

易损/危险品物流监测智能微系统

一种基于数据采集、射频识别的信息采集系统,可以采集存储物流过程中超过阈值的振动、湿度以及温度,并记录对应的时间,然后通过无线通信向外发送记录的数据。本系统由三部分组成,包括基于加速度传感器、温/湿度传感器的数据采集模块、基于RFID的无线通信模块及报警模块。本系统不仅可为易损邮寄物品保驾护航,还可对流通中的危险品状态进行实时监测,能应用于多种恶劣环境,实时将报警消息发送至运输人员手中,及时发现问题,提高运输效率,有效地降低运输货品的破损率和危险品的事故率。     

考虑空气阻力的抛体最大射程和最佳抛射角研究

为了研究抛体在什么抛射角抛出时具有最大射程,利用拉格朗日乘子法,推导出存在空气阻力并且起点和终点不在同一高度时,在某一斜面上抛出的抛体的最大射程和最佳抛射角.通过计算机编程,以计算投掷手榴弹时的最大射程和最佳抛射角为例进行验证,并对物理教学中抛体运动的动力学过程进行了进一步的分析和讨论,有利于提高教学效果.     

红外测速光幕靶改进及测量精度分析

为提高XGK-2002型红外测速光幕靶的测量精度及安装调试速度,提出采用双辅助激光器实现光源和接收精确对准的光幕靶改进方案.在现有红外测速光幕靶工作原理及结构基础上,对光源和接收对准中存在的问题进行了探讨,分析了其影响.提出了在光幕靶两端分别设置一激光器实现对准的光幕靶改进方案,并从测时误差及靶距误差两方面对改进后测量精度进行了分析.结果表明,改进后的光幕靶可快速、直观的实现光源和接收的对准,测试精度及安装可靠性提高,改进后测速精度可达到1‰.     

Analysis Model on Penetration Depth of Concrete by Eroding Long-Rod Projectiles

Mass loss should be considered while calculating the penetration depth of concrete by eroding long-rod projectiles of high velocity.The penetration process is divided into two phases:eroding phase and rigid phase.During eroding phase,a model to predict the penetration depth is established on the assumption that there is a chipping region in the bottom of crater.During rigid phase,Forrestal formula is adopted to calculate the penetration depth.Using this model,the depth of concrete penetration by a tungsten alloy long-rod projectile is calculated.When the critical eroding velocity is between 950 m/s and 1 000 m/s,the result is in good agreement with the experimental data.     

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.     

Sliding mode disturbance observer-based backstepping control for a transport aircraft

This paper presents a novel control method by integrating the sliding mode disturbance observer- based control and the backstepping control technique, and successfully applies it to a flight control system for heavy cargo airdrop operations. The super-twisting second order sliding mode disturbance observer （SOSMDO） is employed to estimate bounded but otherwise arbitrary disturbances, thus ensuring asymptotic convergence of the estimation error to zero in a finite time. Besides, the integrated controller can significantly improve the robustness of the flight control system to modeling uncertainty and external disturbance in the presence of state/control constraints. The closed-loop stability is guaranteed in the sense of Lyapunov. In addition, the proposed approach can considerably reduce design cycles. The performance of the proposed control method is demonstrated in a very low altitude extraction airdrop simulation with a high-fidelity six-degree-of-freedom transport aircraft model.     

超高速弹丸膛口流场结构分析

为了计算和分析超高速弹丸膛口流场的分布状况,建立了超高速弹丸从膛底飞离出炮口整个过程的膛口流场二维轴对称数值仿真模型.基于有限体积法,采用分块网格划分的整体运动处理方法,结合结构动网格技术及Realizable k-ε湍流模型,耦合内弹道及后效期过程,利用六自由度运动方程控制弹丸运动,以300 mm平衡炮为例,研究了1 730 m/s发射速度下的超高速膛口流场特性.计算结果表明:超高速运动的弹丸在距膛口3.3 m远处便形成了清晰的初始流场,弹前激波到达炮口处压力达到了3.8 MPa左右.喷射出的火药燃气速度达到2 500 m/s,但火药燃气仍未能追赶并包围弹丸,因此膛口流场对超高速弹丸运动的影响不同于对中低速弹丸运动的影响;膛口形成了由冠状冲击波、弹底激波、反射激波、马赫盘构成的多层次激波、间断面相互叠加的完整波系,该发射条件下的膛口流场异常强烈,波系结构更加明显.