侧壁式气垫船水压场数值计算

建立了侧壁式气垫船水压场计算的物理和数学模型,并提出了相应的求解方法．在侧壁高度与水深之比较小时,进行了数值求解,并将计算结果与实验作了比较,两者符合较好．     

固体零温零压密度的估算

固体在零温零压下的密度是一个重要的物态参数。本文利用Ｄｅｂｙｅ理论给出了零温零压密度的一种估算方法,并对８２种物质的零温零压密度进行了计算。     

细长船对中深水底引起的动水压力系数计算

文献对水压场的基本方程进行分析,得出了水压场的“浅水理论”。本文用它对中深水细长船水压场某些方面进行分析,即用它对中深水细长船水压场进行计算(船的正下方除外)和对不同水底深度的动水压力系数进行换算。两者所得结果在亚临界流动范围内均较为满意。     

IN SEARCH OF THE AVERAGE TRANSNATIONAL TERRORIST ATTACK VENUE

In this paper we develop an empirical model for transnational terrorist activity for a panel consisting of 139 countries over the period 1985–1998. Essentially, we attempt to sketch the profile of the average terrorist attack venue. Our findings suggest that the terrorist attack venue is, on average, characterized by low economic openness, high demographic stress, and a high level of international disputes. Furthermore, we document a strong regional component suggesting the presence of infectious contagion on a spatial level. Our results also support the presence of addictive contagion captured by a strong autoregressive component in each country’s terrorist activity. Finally, we find a weak statistical link between the level of democracy and terrorist activity, although the level of democracy is a significant determinant of the potential under‐reporting bias of terrorist activity.     

气缸张开式尾翼弹气缸压力数值仿真研究

为研究气缸张开式尾翼工作原理,分析某型滑膛反坦克炮榴弹气缸充放气过程,建立尾翼弹在炮膛内的气缸压力模型,将其与炮弹底部气体压力、密度、温度等参量的变化规律相耦合,并对气缸压力模型进行可解性分析,得到一种求解气缸气体压力、密度等参数随时间变化的数值方法．     

内腐蚀缺陷尺寸对DN150承插管线承压能力的影响

为了科学地指导DN150承插管线的使用与管理,采用非线性有限元法对带内腐蚀缺陷的DN150承插管线进行了剩余强度的评估。通过分析和计算,研究了腐蚀缺陷宽度、长度和深度对管线极限承载能力的影响。结果表明：腐蚀缺陷宽度对DN150承插管线的承载能力影响很小,可忽略不计;随着腐蚀缺陷长度的增加,管线的承载能力略微减小,当缺陷长度达到150mm,管道失效压力基本不变;随着腐蚀缺陷深度的增加,管道失效压力呈线性递减,其对管道失效压力的影响程度远远大于腐蚀缺陷长度。     

甲B类液体全压力储罐消防设计问题研究

对沸点低于45℃的甲B类液体全压力储罐消防设计、审查过程中存在的问题进行了较为全面的分析,并针对这些问题提出了解决的方法,为进一步完善相关工程设计规范和有效地执行这些规范提供了实例,以期给同类工程提供有益借鉴.     

The properties of Sn–Zn–Al–La fusible alloy for mitigation devices of solid propellant rocket motors

The Al and La elements are added to the Sn9Zn alloy to obtain the fusible alloy for the mitigation devices of solid propellant rocket motors. Differential scanning calorimetry (DSC), metallographic analysis, scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), tensile testing and fracture analysis were used to study the effect of Al and La elements on the microstructure, melting characteristics, and mechanical properties of the Sn9Zn alloy. Whether the fusible diaphragm can effectively relieve pressure was investigated by the hydrostatic pressure at high-temperature test. Experimental results show that the melting point of the Sn9Zn-0.8Al0·2La and Sn9Zn–3Al0·2La fusible alloys can meet the predetermined working temperature of ventilation. The mechanical properties of those are more than 35% higher than that of the Sn9Zn alloy at −50 °C–70 °C, and the mechanical strength is reduced by 80% at 175 °C. It is proven by the hydrostatic pressure at high-temperature test that the fusible diaphragm can relieve pressure effectively and can be used for the design of the mitigation devices of solid propellant rocket motors.     

Experimental study on the cavity evolution and liquid spurt of hydrodynamic ram

In research of the characteristics of the cavity evolution, the pressure, and the liquid spurt in hydrodynamic ram, the experiment of the high-velocity fragment impacting the water-filled container had been conducted. The relationships between the above three characteristics have been researched. The evolution of the cavity can be divided into three processes according to its shape characteristics. The first liquid spurt occurred in Process Ⅱ and the rest of it occurred in Process Ⅲ. The duration of the second liquid spurt is longer than the first liquid spurt. When the impact velocity of the fragment is less than 996 m/s, the velocity of the second liquid spurt is the highest. When the velocity of the fragment is greater than 996 m/s, the velocity of the first liquid spurt is the highest. The maximum velocities of the first and second liquid spurt are 111 m/s and 94 m/s respectively. The pressure fluctuated sharply in Processes Ⅰ and Ⅲ. The maximum peak pressures in the shock and the cavity oscillation phases are 15.51 MPa and 7.96 MPa respectively. The time interval of the two adjacent pressure pulses increases with the increase of the fragment velocity.     

高亚声速时叶尖小翼对压气机叶栅泄漏流动的影响

为了探索跨声速来流条件时,不同安装位置、不同宽度的叶尖小翼对压气机叶栅气动特性的影响,对Ma=0.8时包括原型叶栅在内的7种扩压叶栅的流场进行了数值研究.结果表明:在多种因素的共同影响下,不同来流冲角的吸力面叶尖小翼在流场中都为负效果,增加了流场复杂性;压力面叶尖小翼则改善了泄漏流动,减小了流动损失.两种安装位置的叶尖...