飞片冲击起爆炸药的爆炸判据研究

对飞片冲击起爆炸药的爆炸判据进行了研究．提出了用1／2铝鉴定块凹痕深度作为飞片冲击起爆炸药的爆炸判据的方法,简单而又合理．进行了3种炸药的飞片感度的测定．在相同的实验条件下,炸药PETN,HMX,HNS的飞片感度的排序为PETN〉HMX〉HNS．     

飞片碰靶产生冲击波的简化模型

提出了一种计算飞片靶产生冲击的增长与衰减规律的简单方法,采用该方法计算了具有密度和速度空间分布的铝飞片碰撞静止铝平面靶驱动的冲击波在靶中的增长与衰减的情况,并与我们在大型计算机上的数值模拟结果进行了比较.     

Cavitation Inception in Turbulent Flows Around a Hydrofoil

For most engineering purposes cavitation de-grades performance.Engineering designs are ai med atproducing geometries and operating conditions thatresist cavitation.It is desirable to identify,under-stand,predict,and control the physical mechanismsleading to cavitation inception.One of the centralproblems in cavitation research has been the predic-tion of the onset or inception of cavitation.The cavi-tation occurring in a flow system is related to thepressure field and viscous flowpatterns[1].…     

Numerical simulation for deformation of multi-layer steel plates under underwater impulsive loading

To further understand the dynamic deformation and impact resistance of thin-plate hull structure under impulse wave,the deformation of multi-layer steel plates under underwater impulsive loading has be...     

Investigation on extremal and critical characteristics of ignition time for H_2/O_2 combustion system and their applications

The L,H and C curves in P-T phase are proposed to describe the minimal,maximal and critical char-acteristics of ignition time of H2/O2 combustion system,respectively.The features of H2/O2(Air) com-bustion system,including explosion or not as well as the time delay to achieve its explosion status,can be well shown by explosion limits and these proposed curves.These curves can be described by 1.2k1=ks[Ms],(k11/k10+1)k1=ks[Ms],and 2k1=ks[Ms],respectively,which provide a physical explanation for these curves an...     

Numerical simulation for explosion wave propagation of combustible mixture gas

A two-dimensional multi-material code was indigenously developed to investigate the effects of duct boundary conditions and ignition positions on the propagation law of explosion wave for hydrogen and methane-based combustible mixture gas. In the code,Young’s technique was employed to track the interface between the explosion products and air,and combustible function model was adopted to simulate ignition process. The code was employed to study explosion flow field inside and outside the duct and to obtain peak pressures in different boundary conditions and ignition positions. Numerical results suggest that during the propagation in a duct,for point initiation,the curvature of spherical wave front gradually decreases and evolves into plane wave. Due to the multiple reflections on the duct wall,multi-peak values appear on pressure—time curve,and peak pressure strongly relies on the duct boundary conditions and ignition position. When explosive wave reaches the exit of the duct,explosion products expand outward and forms shock wave in air. Multiple rarefaction waves also occur and propagate upstream along the duct to decrease the pressure in the duct. The results are in agreement with one-dimensional isentropic gas flow theory of the explosion products,and indicate that the ignition model and multi-material interface treatment method are feasible.     

封闭空间瓦斯爆炸过程的反应动力学分析

为了获取瓦斯爆炸过程中反应动力学参数,通过修改化学动力学计算软件CHEMKINIII中的SENKIN程序包,采用甲烷燃烧的化学动力学详细反应机理(包括16种组分、41个反应),建立了定容弹中瓦斯爆炸过程的计算模型.利用该模型对瓦斯爆炸过程中温度、压力及反应物浓度的变化趋势进行了模拟分析,同时通过对瓦斯爆炸详细反应机理的敏感性分析,找出了影响瓦斯爆炸以及爆炸后部分致灾性气体生成的关键反应步.结果表明:瓦斯爆炸后温度、压力将分别达到2800K,0.24MPa左右;促进瓦斯爆炸的关键反应步为CH3+O2=CH3O+O,CH4+HO2=CH3+H2O2;促进CO与CO2生成的关键反应步为CH3+O2=CH3O+O,CH4+O2=CH3+HO2,CH4+HO2=CH3+H2O2,CH3+HO2=CH3O+OH,H+O2=OH+O.     

Numerical Simulation of the Protective Effect of Complex Boundaries Toward Shock Waves in a 3D Explosive Field

A numerical method is presented that simulates 3D explosive field problems.A code MMIC3D using this method can be used to simulate the propagation and reflected effects of all kinds of rigid boundaries to shock waves produced by an explosive source.These numerical results indicate that the code MMIC3Dhas the ability in computing cases such as 3D shock waves produced by air explosion,vortex region of the shock wave,the Mach wave,and ceflected waves behind rigid boundaties.     

海船法向靠岸速度数字模拟

根据海船中较为典型的船型（1－5万t)的法向靠岸速度实测子样,采用蒙特卡洛法,通过计算机随机实验对其法向靠岸速度进行随机模拟,并经过统计检验求出法向靠岸速度最大值的分布和最大值的失效概率曲线;并与现行港口工程技术规范建议值及有关资料进行了比较。     

Numerical Simulation on Explosion in Double-Layer Medium of Concrete and Soil

The numerical simulation on explosion in concrete and soil is performed by using the three-dimension finite element code LS-DYNA, into which a continuum damage model which can well describe the fracture of concrete is implemented. As a consequence, wave propagation and attenuation in concrete and on soil-concrete interface are obtained respectively. Moreover, the damage regions of concrete at different thicknesses of soil （TOS） and depths of charge （DOC） are procured. The existent soil reduces damage region of concrete. Numerical results provide reference for design of warhead and protective structure and blasting.     

Numerical Simulation on Explosion in Double-Layer Medium of Concrete and Soil

The numerical simulation on explosion in concrete and soil is performed by using the three-dimension finite element code LS-DYNA, into which a continuum damage model which can well describe the fracture of concrete is implemented. As a consequence, wave propagation and attenuation in concrete and on soil-concrete interface are obtained respectively. Moreover, the damage regions of concrete at different thicknesses of soil (TOS) and depths of charge (DOC) are procured. The existent soil reduces damage region of concrete. Numerical results provide reference for design of warhead and protective structure and blasting.     

Investigation on extremal and critical characteristics of ignition time for H<Subscript>2</Subscript>/O<Subscript>2</Subscript> combustion system and their applications

The L, H and C curves in P-T phase are proposed to describe the minimal, maximal and critical characteristics of ignition time of H₂/O₂ combustion system, respectively. The features of H₂/O₂(Air) combustion system, including explosion or not as well as the time delay to achieve its explosion status, can be well shown by explosion limits and these proposed curves. These curves can be described by 1.2k ₁=k _s [M_s], (k ₁₁/k ₁₀+1)k ₁=k _s [M_s], and 2k ₁=k _s [M_s], respectively, which provide a physical explanation for these curves and give another way to establish them. Based on the contour of ignition time, the Z-type explosion limits can be explained by thermal explosion theory. Furthermore, the ignition distance of supersonic combustion is predicted according to the ignition time obtained in a Semenov system, which is very reasonable.     

非定常拍动翼的水动力性能研究

拍动翼推进方式为水下机器人推进提供了更有效地选择,为了探究拍动翼的水动力性能,采用基于速度势的面元法对非定常拍动翼在特定运动规律下产生的水动力进行了计算,通过与相关实验数据的对比,同时采用计算流体力学FLUENT软件进行了计算并且将结果进行比较,结果的变化趋势一致,最小误差只有11%,充分验证了面元法计算的可靠有效性.通过对拍动翼水动力计算结果的研究,分析了各个运动参数包括来流速度、运动幅值、相位差和运动频率对拍动翼水动力性能的影响.     

受限空间瓦斯爆炸火焰与毒气传播研究

为揭示瓦斯爆炸过程中火焰、毒气及压力三者间相互关系,采用一端封闭的爆炸试验装置,通过改变瓦斯聚集长度和点火强度,研究了瓦斯爆轰及爆燃状态下火焰、毒气及压力传播变化规律.结果表明,管道内瓦斯爆燃状态下火焰的传播速度远小于爆轰状态下的传播速度,变化趋势呈线性;瓦斯爆炸火焰传播速度的大小直接影响爆轰的形成以及爆炸强度和爆炸传播距离;爆燃状态下火焰和毒气传播的距离基本相当,均为原始瓦斯聚集总长度的2倍左右;爆轰状态下火焰和毒气传播的距离基本相当,均大于原始瓦斯聚集长度,但传播距离不确定.     

煤粉—惰性介质混合体系爆炸特性实验研究

为深入认识煤粉—惰性介质混合体系爆炸行为,在Siwek 20 L球形爆炸测试系统内研究了煤粉—惰性介质混合体系的爆炸威力(最大爆炸压力、最大升压速率、燃烧持续时间)、敏感度(爆炸上、下限)和惰性介质的抑爆效力,并重点考察了点火能量、煤粉热值、惰性介质组分、煤粉浓度、煤/惰性介质混合比等因素的影响。结果表明,添加惰性介质能显著降低煤粉爆炸威力,其抑爆效力随点火能量增加而下降,并由此建议采用5～10 kJ点火能量考察惰化效应;煤粉热值增加可显著提高混合体系的爆炸威力;就惰化效应而言,湿分的抑爆效力优于磷酸二氢铵和碳酸钙,而磷酸二氢铵的抑爆效力又优于碳酸钙,其中煤粉完全惰化所需惰化剂量与煤尘浓度密切相关,在200～400 g/m3处有最大值,为"最危险浓度";增加惰性介质添加量可降低爆炸上限,提高爆炸下限,有效压缩煤粉尘可爆浓度范围。研究结果对深入理解粉尘爆炸规律、优化惰化标准,完善测试方法有参考价值。     

动载荷作用下HR-2钢的层裂特性

利用轻气炮加载技术和VISAR（激光速度干涉仪）光测技术，在500m／s的冲击加载速度下，对3种不同厚度的HR-2抗氢钢样品进行了层裂实验，得到样品自由面速度剖面曲线。根据所得曲线波形计算出相应条件下的层裂强度、层裂片厚度以及各自的应变率，最后得到层裂强度随拉伸应变率变化的关系曲线。通过实验与分析可知，在相同冲击压力下，层裂强度随拉伸应变率的增长而增长，随样品厚度的增加而减小。     

粗纱机传动系统的改进

针对粗纱机传动系统过于复杂，控制精度低，动态响应性能差等缺点，应用机电一体化技术，提出了采用微型计算机控制，变频调速四电机驱动的新型粗纱机设计方案。并对该新型粗纱机的机械传动系统和电气控制系统进行了设计，同时给出了实现计算机控制的工艺数字模型。     

Experimental Study and Numerical Simulation of Hypervelocity Projectile Impact on Double-Wall Structure

Tests of hypervelocity projectile impact on double-wall structure were performed with the front wall ranging from 0.5 mm to 2.0 mm thick and different impact velocities. Smooth particle hydrodynamics (SPH) code in LS-DYNA was employed for the simulation of hypervelocity impact on the double-wall structure. By using elementary shock wave theory, the experimental results above are analyzed. The analysis can provide an explanation for the penetration mechanism of hypervelocity projectile impact on double-wall structure about the effect of front wall thickness and impact velocity.     

小型飞行器定位的数据融合误差修正方法

给出了一种小型飞行器定位误差修正方法。由飞行器运动方程,推导出了斜距和飞行状态之间的关系,根据所测得的飞行状态,利用Kalman滤波方法可得斜距估计。根据实测值、最优估计值和GPS推算值进行数据融合,进一步对无线电仪表定位误差进行修正,仿真和数据回放结果表明,使用此方法可以得到飞行器更准确的定位。     

三角形蜂窝的共面冲击动力学

采用有限元方法研究了冲击速度在3-250m／s的条件下,结构参数和冲击速度对三角形蜂窝共面冲击力学性能的影响．三角形蜂窝在不同冲击速度下呈现不同的变形模式,各变形模式间的转换速度随着壁厚边长比和扩展角的增加而增加．当所有结构参数保持恒定时,共面动态峰应力与冲击速度的平方呈线性关系．对于给定的冲击速度,共面动态峰应力与壁厚边长比成幂指数关系,与扩展角的关系可以用一较复杂的数学模型进行拟合．基于有限元计算结果利用最小二乘法拟合得到了共面动态峰应力关于各结构参数和冲击速度的经验关系式．