Efficient initiation of detonation waves is the key to the pulse detonation engine AB.
有效的触发爆震波是脉冲爆震发动机正常工作的关键所在。
The propagation of one dimensional divergent detonation waves is studied in this paper.
本文研究一维散心爆轰波的传播规律。
As an example, the isobars are plotted for strong detonation waves passing over a wedge surface.
作为例子，文中计算了强爆震波绕薄楔时的等压线。
An analytical solution is obtained for the diffraction of strong detonation waves by a stationary two-dimensional thin airfoil.
本文研究平面强爆震波对静止的零攻角二维对称薄翼的绕射问题，并求得解析解。
There are two methods, analytical and graphical, in calculating the interaction of detonation waves with a non-reactive medium.
爆轰波与惰性介质相互作用的计算。可以用解析解和作图法求解。
The present experimental investigation attempts to understand the propagation of gaseous detonation waves in a section lined with perforated steel plate.
本实验旨在研究气相爆轰波在衬有多孔钢板的管道中传播的现象。
The present experimental investigation attempts to understand the attenuation of detonation waves propagating through an absorbing material lining section.
实验旨在研究气相爆轰波在阻尼管道（管壁上衬有吸收材料）中传播时的衰减现象。
A pulse detonation rocket engine (PDRE) is a new propulsion system that generates thrust by using high-temperature and high-pressure air produced by pulse detonation waves.
脉冲爆震火箭发动机是一种利用脉冲式爆震波产生高温、高压燃气发出的冲量来产生推力的新型推进系统。
A simple approximate calculation method is given, which can exactly reconstruct the long distance non ideal propagation of detonation waves in the spherical shell of the charge.
针对实验结果给出一种简便的近似计算方法，它能准确地重现炸药球壳中长程绕射爆轰波的非理想传播行为。
The detonation was fully established through a series of interactions and impacts of reflected shock waves.
激波爆震波转捩是快点火过程，是爆震波建立的一个非常重要的机理。
After gaseous detonation reflects on the right wall, the right-traveling rarefaction waves accelerate the reflected shock.
气相爆轰波在右壁面反射后，右行稀疏波加速反射激波。
The computational results show that the waves system is complex during detonation traveling inside tube.
计算结果显示，爆轰波在管内传播时，其波系极其复杂。
The computational results show that the waves system is complex during detonation traveling inside tube.
计算结果显示，爆轰波在管内传播时，其波系极其复杂。
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