一种新型防护结构对爆炸冲击波衰减特性的研究

运用大型有限元软件LS—DYNA,在相同爆炸冲击波作用下,对洞库口部普通钢板防护门和有泡沫铝夹层的钢板防护门两种防护结构的隔爆性能进行了数值模拟和对比分析,结果表明:有泡沫铝夹层的钢板防护门对爆炸冲击波有着良好的衰减特性。同时表明该新型防护结构对洞库口部抗爆炸冲击波设计有着很高的参考价值。     

高透波性大刚度桅杆设计与性能测试分析

提出了用复合材料技术设计与制造高透波性大刚度桅杆的方法,以高强玻璃纤维为增强材料、SW905乙烯基脂树脂为基体材料,制作出1∶1桅杆模型,对制作出的桅杆模型进行了性能测试.测试结果表明,制作出的桅杆具有高透波性和较大的动刚度.     

合成孔径声纳的数学问题

根据波动方程线性化模型,考虑了合成孔径成像的数学问题,对于在二维曲面上所获得的数据来重建三维景物,将基阵的运动和旋转归结为对基阵轨迹的依赖上.利用微局部分析给出了一般问题的一种新的理论反演算法,并且分析了成像系统的分辨率,从而为今后的工作打下理论基础.     

无人炮塔系统关键技术组合分析

无人炮塔系统是未来火力系统发展的方向,在坦克和装甲车辆炮塔部分被命中概率高的现实情况下,无人炮塔对乘员来说相对安全。文章初步分析了无人炮塔系统的关键技术——遥控火炮技术和自动输弹技术实现的可能性和途径,并且针对在相同底盘上配置更大威力火炮的要求,探讨了膨胀波技术在无人炮塔上的应用。     

基于MIDAS的大跨度斜拉桥行波效应分析

针对宜巴段三塔四跨斜拉桥工程实例,结合MIDAS软件,进行动态时程分析,对比研究了行波效应对桥塔、桥墩各控制点的位移、剪力以及轴力的纵向地震反应的影响。通过施加-EL-Centro纵向地震波作用,模拟出斜拉桥控制点的位移、内力地震反应最大值,得出结论：对于多塔斜拉桥,行波效应对各桥塔塔底、各桥塔塔顶内力、位移响应的影响不同。     

油料火灾爆炸模拟实验系统与测试技术

针对受限空间油料火灾爆炸发生、发展、控制、抑制实验的需要,研制了一系列模拟实验台架及关键参数测试系统。所研制的一系列模拟实验台架为各种工况的油料火灾爆炸模拟实验研究提供了完备的科研条件和支撑;研制的超动态数据采集与分析系统能对冲击波压力、瞬时温度、火焰识别、爆燃向爆轰演化(DDT)过程等进行连续捕捉、测试、分析;研制的基于紫外火焰探测、数字信号处理和网络化智能探测技术的油气爆炸火焰传播速度测试系统较传统的火焰传感器具有高灵敏度、零误报、探测距离远的特点。     

基于AHP的舰船大风浪中航行安全评价

舰船在大风浪中航行的风险是一个比较重要的研究领域,其风险程度很难用量化进行评估.为了更好地方便研究,并为以后的研究奠定理论基础,采用了层次分析法,建立舰船在大风浪中航行的安全评价体系,同时构造了判断矩阵,并进行了层次单排序一致性检验,求出了每个影响舰船航行安全因素的权重,并通过实例进行解算,得出结果和实际情况相比大致相似.此方法可以较好地对舰船在大风浪中航行的安全进行直观的描述,可供舰船长用来掌握舰船航行的风险情况,进而进行有效的风险决策.     

Numerical simulation of the blast wave of a multilayer composite charge

The numerical simulation of a blast wave of a multilayer composite charge is investigated. A calculation model of the near-field explosion and far-field propagation of the shock wave of a composite charge is established using the AUTODYN finite element program. Results of the near-field and far-field calculations of the shock wave respectively converge at cell sizes of 0.25–0.5 cm and 1–3 cm. The Euler––flux-corrected transport solver is found to be suitable for the far-field calculation after mapping. A numerical simulation is conducted to study the formation, propagation, and interaction of the shock wave of the composite charge for different initiation modes. It is found that the initiation mode obviously affects the shock-wave waveform and pressure distribution of the composite charge. Additionally, it is found that the area of the overpressure distribution is greatest for internal and external simultaneous initiation, and the peak pressure of the shock wave exponentially decays, fitting the calculation formula of the peak overpressure attenuation under different initiation modes, which is obtained and verified by experiment. The difference between numerical and experimental results is less than 10%, and the peak overpressure of both internal and external initiation is 56.12% higher than that of central single-point initiation.     

Experimental research on the instability propagation characteristics of liquid kerosene rotating detonation wave

In order to study the instability propagation characteristics of the liquid kerosene rotating detonation wave (RDW), a series of experimental tests were carried out on the rotating detonation combustor (RDC) with air-heater. The fuel and oxidizer are room-temperature liquid kerosene and preheated oxygen-enriched air, respectively. The experimental tests keep the equivalence ratio of 0.81 and the oxygen mass fraction of 35% unchanged, and the total mass flow rate is maintained at about 1000 g/s, changing the total temperature of the oxygen-enriched air from 620 K to 860 K. Three different types of instability were observed in the experiments: temporal and spatial instability, mode transition and re-initiation. The interaction between RDW and supply plenum may be the main reason for the fluctuations of detonation wave velocity and pressure peaks with time. Moreover, the inconsistent mixing of fuel and oxidizer at different circumferential positions is related to RDW oscillate spatially. The phenomenon of single-double-single wave transition is analyzed. During the transition, the initial RDW weakens until disappears, and the compression wave strengthens until it becomes a new RDW and propagates steadily. The increased deflagration between the detonation products and the fresh gas layer caused by excessively high temperature is one of the reasons for the RDC quenching and re-initiation.     

Analysis of the stress wave and rarefaction wave produced by hypervelocity impact of sphere onto thin plate

Shock wave is emitted into the plate and sphere when a sphere hypervelocity impacts onto a thin plate. The fragmentation and phase change of the material caused by the propagation and unloading of shock wave could result in the formation of debris cloud eventually. Propagation models are deduced based on one-dimensional shock wave theory and the geometry of sphere, which uses elliptic equations (corresponding to ellipsoid equations in physical space) to describe the propagation of shock wave and the rarefaction wave. The “Effective thickness” is defined as the critical plate thickness that ensures the rarefaction wave overtake the shock wave at the back of the sphere. The “Effective thickness” is directly related to the form of the debris cloud. The relation of the “Effective thickness” and the “Optimum thickness” is also discussed. The impacts of Al spheres onto Al plates are simulated within SPH to verify the propagation models and associated theories. The results show that the wave fronts predicted by the propagation models are closer to the simulation result at higher impact velocity. The curvatures of the wave fronts decrease with the increase of impact velocities. The predicted “Effective thickness” is consistent with the simulation results. The analysis about the shock wave propagation and unloading in this paper can provide a new sight and inspiration for the quantitative study of hypervelocity impact and space debris protection.