爆轰波,detonation wave
1)detonation wave爆轰波
1.Influences of particle size of HMX ondetonation waves propagation of HMX and HMX/F_(2641);HMX粒度与爆轰波传播性能的关系研究
2.Numerical simulation of standing obliquedetonation wave using parallel computation method;驻定斜爆轰波并行数值模拟
3.Numerical simulation of gaseousdetonation waves propagation and comparison with experimental results;气相爆轰波传播特性的数值模拟及实验对照
英文短句/例句
1.EXPERIMENTAL INVESTIGATIONS OF THE MACH REFLECTION IN A CONDENSED EXPLOSIVE凝聚炸药中爆轰波马赫反射的实验研究
2.Influences of microstructure on detonation-spreading performances of TATB-based explosivesTATB微观结构对炸药爆轰波传播性能的影响
3.Effects of Focusing Angle on Laser-supported Detonation Wave in Air聚焦角度对空气中激光维持爆轰波的影响
4.Temperature Measurement of Laser-Induced Plasma Detonation Wave激光支持等离子体爆轰波温度的实验测量
5.Numerical Simulation of the Diffraction Detonation Wave Based on the Modified SPH Method基于修正SPH方法的爆轰波绕射传播的数值模拟
6.Research and Application the Radial Detonating Explosives in the Hole Detonation Wave Propagation Direction;孔内炸药径向起爆爆轰波传播方向的研究及应用
7.An experimental investigation is presented concerning the re-intension process of a detonation wave occurring downstream of the acoustic absorbing walled section in this paper.实验研究了爆轰波在声学吸收段下游发生的再恢复过程。
8.TWO DIMENSIONAL NUMERICAL SIMULATION FOR THE INERTIAL EFFECT OF EMV GAUGE MOVING WITH DETONATION WAVE电磁量计随爆轰波运动惯性性质的二维数值模拟
9.The Numerical Method and Simulation for Propagating Front of Non-Ideal 3D Detonation;三维非理想爆轰波阵面传播过程的数值方法和数值模拟
10.Experimental Study on Dynamic Behavior of Lead Plate Driven by Two Head-on Colliding Detonation Waves爆轰波对碰驱动下平面铅飞层对碰区动载行为实验研究
11.This paper presents a method of characteristics to calculate the structure of the detonation wave in condensed explosive by the decay shock curve data obtained in the aquarium test.提出了一种利用爆轰波垂直入射时水中冲击波的衰减曲线计算凝聚炸药爆轰波剖面的特征线方法。
12.As an example, the distribution of the detonation pressure, density, particle and sound velocity along the detonation profile are given for TNT.以TNT为例进行了计算,给出了其爆轰波内压力、度、速和声速等参数的分布。
13.Numerical Simulation of Metallic Sphere-shell"s Pressure Caused by Detonation Wave Based on Modified SPH基于修正光滑粒子流体动力学的爆轰波对金属球壳的压强数值模拟
14.Numerical Simulation Shock Wave Exteral Flow of Pulse Detonation Engine脉冲爆轰发动机冲击波外流场数值模拟
15.A acoustooptic switch for shock wave and detonation physics experiments用于冲击波和爆轰物理实验中的声光开关
16.Investigation of detached detonation induced by oblique shock in premixed supersonic flow预混超声速气流斜激波诱导脱体爆轰研究
17.Boom! Boom! Boom! A series of explosions shook the valley.轰！轰！轰！一连串爆破声震撼山谷。
18.detonation limit for mixture gases可燃混合气的爆轰范围
相关短句/例句
detonation[英][,det?"ne??n][美]["d?t?"ne??n]爆轰波
1.Numerical investigation ofdetonation direct initiation induced by toroidal shock wave focusing;用环形激波聚焦实现爆轰波直接起爆的数值模拟
2.Study on thedetonation cellular structure of propylene epoxide-Air;环氧丙烷-空气混合物爆轰波胞格结构的研究
3.A numerical investigation on the performance of a backward-forward double-detonation driver for high enthalpy shock tubes was conducted by solving one-dimensional Euler equations with the Dispersion Controlled Dissipative (DCD) scheme.当初始压力比大于临界值时,在主驱动段中能产生过驱动爆轰波,不仅Taylor波被完全消除,而且驱动能力较单一前向爆轰驱动段强。
3)detonation waves爆轰波
1.It is important to study the ignition,growth and propagation of the laser supporteddetonation waves.采用高速纹影摄影法记录激光支持等离子体爆轰波流场的演化,得到流场冲击波阵面形状和尺寸随时间变化规律。
2.In order to carry out an investigation for the influence of physical and geometricl boundary conditions on the propagation of gaseousdetonation waves, a double walled detonation shock tube (40×40mm square section) on hand is reconstructed.为开展边界物理和几何条件对气相爆轰波传播影响的系统研究，需要对已有的４０×４０ｍｍ方截面双层爆轰激波管进行改造。
3.The results of experiment and theoretical analysis are show that the defects occurred in interface is related to the orientation ofdetonation waves propagating and the open position of gap pillars,and that the defects can be eliminated or reduced.通过理论分析,验证了此类缺陷的产生和间隙开口方位相对于爆轰波传播方向有关,消除或减小了缺陷的发生机率。
4)oblique detonation斜爆轰波
1.This paper presents the experimental results of the initiation and stabilization of anoblique detonation by launching a hypervelocity projectiles at velocities of 1700～2100m/s,into H 2 air mixtures.给出了锥形弹丸以 16 0 0～ 2 10 0m/s的速度射入预混的氢 空气混合介质中形成驻定斜爆轰波的试验结果 ,并讨论锥顶角、飞行体速度以及可燃介质当量比等因素对形成驻定斜爆轰波的影
2.Theoblique detonation stabilized on a hypervelocity projectile was researched by numerical simulations and experimental visualizations.通过数值模拟和实验显示的方法对驻定在高速飞行体上斜爆轰波流场进行研究。
5)Detonation (DT) wave爆轰(DT)波
6)initiation modes爆轰波形
延伸阅读
轰5
轰5
轰-5(h-5或b-5)是中国哈尔滨飞机公司参照苏联的伊尔-28轰机改进设计并试制生产的一种亚音速轻型轰炸机，可在各种复杂的气象、地理条件下执行战术轰炸及攻击任务。1963年1月开始基本型的试制准备，1966年9月首次试飞，1967年投入批量生产，1984年停产。该机现已基本退出现役。该机有多种改型，各型情况如下：轰-5，基本型；轰-5甲，改进型，航程增加并缩短了起飞滑跑距离；轰-5鱼雷型，可挂鱼雷和副油箱；轰侦-5，是在轰-5基础上改装照相侦察设备而成的侦察机，比基本型航程增大；轰教-5，轰炸教练型。主要机载设备轰炸雷达，自动领航仪，敌我识别器及各种通讯导航设备等。动力装置两台wp-5甲型涡喷发动机，单台推力 26.48千牛（2700公斤）。武器装备炸弹舱藏在机身中部，机头一门固定23mm航炮，机尾两门活动23mm航炮，总备弹量为650发。尺寸数据机长：16.77米机高：6.20米翼展：21.45米机翼面积：60.8平方米主轮距：7.4米前主轮距：6.67米重量 空重：12890千克正常起飞重量：18400千克最大起飞重量：21200千克机内载油量：3800千克正常动弹量：1000千克最大载弹量：3000千克性能数据 最大平飞速度(高度4500米)：902公里/小时巡航速度：(高度5000米)696公里/小时，(高度10000米)559公里/小时实用升限：12500米最大航程：2400公里起飞滑跑距离：980米着陆滑跑距离：930米轰-5机组包括3名乘员，领航员舱在机头，驾驶员在其身后气泡形驾驶舱内。机尾有与前方不连通的通信射击员舱。我军轰-5未见有装载核武器，可能与当时我国尚无法研制小型核武器有关。翼下还有8个挂架，可挂火箭弹或炸弹。
