Effects of total pressures and equivalence ratios on kerosene/air rotating detonation engines using a paralleling CE/SE method

In this paper, the kerosene/air rotating detonation engines(RDE) are numerically investigated, and the emphasis is laid on the effects of total pressures and equivalence ratios on the operation characteristics of RDE including the initiation, instabilities, and propulsive performance. A hybrid MPI + OpenMP parallel computing model is applied and it is proved to be able to obtain a more effective parallel performance on high performance computing(HPC) systems. A series of cases with the total pressure of 1 MPa, 1.5 MPa, 2 MPa, and the equivalence ratio of 0.9, 1, 1.4 are simulated. On one hand, the total pressure shows a significant impact on the instabilities of rotating detonation waves. The instability phenomenon is observed in cases with low total pressure (1 MPa) and weakened with the increase of the total pressure. The total pressure has a small impact on the detonation wave velocity and the specific impulse. On the other hand, the equivalence ratio shows a negligible influence on the instabilities, while it affects the ignition process and accounts for the detonation velocity deficit. It is more difficult to initiate rotating detonation waves directly in the lean fuel operation condition. Little difference was observed in the thrust with different equivalence ratios of 0.9, 1, and 1.4. The highest specific impulse was obtained in the lean fuel cases, which is around 2700 s. The findings could provide insights into the understanding of the operation characteristics of kerosene/air RDE.     

Transverse relaxation characteristic and stress relaxation model considering molecular chains of HTPB coating based on pre-strained thermal aging

In order to accurately describe the transverse relaxation characteristic and stress relaxation modulus of HTPB coating during pre-strain thermal aging process, a one month thermal aging test was carried out at 70 C with pre-strain of 0％, 3％, 6％ and 9％, respectively. The low-field 1H NMR and stress relaxation modulus tests were carried out for HTPB coating at different aging stages. The stress relaxation model considering the molecular chains was proposed according to the changes of crosslinking chain and dangling chain of HTPB coating during pre-strain aging. The results showed that with the increase of aging time, the decay rate of transverse relaxation curve became faster, the transverse relaxation time decreased, the value of combined parameter qMrl increased, the proportion of crosslinking chain decreased, while the proportion of dangling chain increased. Moreover, the stress relaxation modulus increased, the crosslinking network structure of HTPB coating became denser and the degree of cross-linking increased. At the initial aging stage, the pre-strain will destroy the crosslinking network structure of HTPB coating to a certain extent. With the increase of aging time, the effect of pre-strain will gradually weaken and the influence of aging on materials will gradually increase. The correlations between the stress relaxation model considering the molecular chains and the test results were more than 0.9950, which can accurately describe the stress relaxation modulus of HTPB coating during the pre-strain thermal aging process.     

Effect of metal powders on explosion of fuel-air explosives with delayed secondary igniters

In order to improve the energy level of fuel air explosive(FAE) with delayed secondary igniters, high energetic metal powders were added to liquid fuels mainly composed of ether and isopropyl nitrate. Metal powders' explosive properties and reaction mechanisms in FAE were studied by high-speed video, pressure test system, and infrared thermal imager. The results show that compared with pure liquid fuels, the shock wave overpressure, maximum surface fireball temperature and high temperature duration of the mixture were significantly increased after adding high energetic metal powder. The overpressure values of the liquid-solid mixture at all measuring points were higher than that of the pure liquid fuels. And the maximum temperature of the fireball was up to 1700 ℃, which was higher than that of the pure liquid fuels. After replacing 30％of aluminum powder with boron or magnesium hydride, the shock wave pressure of the mixture was further increased. The high heat of combustion of boron and the hydrogen released by magnesium hydride could effectively increase the blast effect of the mixture. The improvement of the explosion performance of boron was better than magnesium hydride. It shows that adding high energetic metal powder to liquid fuels can effectively improve the explosion performance of FAE.     

武器装备测试系统建设与发展

武器系统在装备部队使用之前,都要经过长时间反复、严格的性能检测和试验,以确保武器系统的先进性和精确性。简要介绍了武器装备测试系统建设概况,阐述了新型武器系统的特点以及对测试系统的要求,重点说明了武器装备测试系统的未来发展重点以及相关的测试系统理论与技术。     

抗美援朝战争中志愿军空军培育战斗精神的历史经验

抗美援朝战争中,志愿军空军在敌强我弱的情况下,既发挥高技术武器装备的作用,又重视战斗精神培育,取得了空战的胜利。他们在培育战斗精神中的“五个结合”,即:把思想教育与技术准备、继承传统与空战实践、单独作战与协同作战、学习苏军与军事民主、立功运动与服务保证结合起来的经验,对当前我军战斗精神的培育具有重要的借鉴意义。     

纳米结构炭材料的储放氢性能研究

主要对多种纳米结构炭材料（超级活性炭、多壁碳纳米管,纳米碳纤堆,纳米石墨纤堆、纳米石墨球等）在常温、10-13MPa的氢气压力下的储放氢量进行了测定（其中包括经过一系列物化处理的样品）,井对其结构和比表面积分别采用SEM、TEM、HRTEM、ASAP2010吸附测试仪（BET）进行了分析．实验结果表明：经过处理的纳米碳样品的储放氢量有所提高,但没有一种样品在温和的实验每件下的储放氢量超过1．0wt％,离DOE目标（6．5wt%）相距甚远。     

储运过程反应失控型火灾爆炸事故的预测与防范

储运化学活泼性物质时易发生反应失控型火灾爆炸事故,其危险性随着容器的增大和储运时间的增长而增加.介绍一种储运容器中反应失控火灾爆炸事故危险性预测的方法,预测结果与实际情况具有良好的一致性,并对预防事故的冷却方法进行了实验研究.     

爆炸沸腾研究进展

分析讨论了液体过热极限、汽泡内压力等爆炸沸腾的重要参数 ,综述了三种主要实验方法 ,提出了有待进一步研究的问题 .     

具有正交(g,f)-因子分解的子图

设G是一个图 ,g (x)和f (x)是定义在V (G)上的整数值函数 ,且对任意的x∈V (G) ,设g (x)≤f (x) ,H是G的一个子图 ,F ={F1,F2 ,… ,Ft}是G的一个因子分解 ,如果对任意的 1≤i≤t,|E (H)∩E (Fi) |=1 ,则称F与H正交。闫桂英和潘教峰在文 [3]中提出如下猜想 :设G是一个 (mg+k,mf-k) -图 ,1≤k相似文献   

二部图的(g,f)匹配

本文证明了二部图存在(g,f)匹配和f 因子的充要条件以及有关的几个结果,并且给出了求二部图的最大(g,f)匹配、最小(g,f)匹配和最小权最大f 匹配、最小权(g,f)匹配、最大权(g,f)匹配的算法。