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1)  potential function of blast wave
爆轰波势函数
2)  parameters of detonation
爆轰波参数
3)  detonation wave
爆轰波
1.
Influences of particle size of HMX on detonation 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 oblique detonation wave using parallel computation method;
驻定斜爆轰波并行数值模拟
3.
Numerical simulation of gaseous detonation 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
4)  detonation [英][,detə'neɪʃn]  [美]['dɛtə'neʃən]
爆轰波
1.
Numerical investigation of detonation 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 the detonation 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。
5)  oblique detonation
斜爆轰波
1.
This paper presents the experimental results of the initiation and stabilization of an oblique 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.
The oblique 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。
6)  Detonation (DT) wave
爆轰(DT)波
补充资料:波势
1.书法指波磔之笔势。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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