Periodicity advance model of 1-d slab symmetry detonation wave is investigated.
一维平面对称爆轰波的推进具有周期性。
Periodicity advance model of 1 - D slab symmetry detonation wave is investigated.
一维平面对称爆轰波的推进具有周期性。
Experimentalresults show that the steadiness and the repeatability of the flow be-hind detonation wave are excellent.
实验结果还表明:爆轰波后气流的定常性和重复性品质优良。
The detonation wave ignition technique is suitable to synchronization ignition of multi-chamber liquid rocket engine.
爆震波多管点火技术适合用于多燃烧室液体火箭发动机的同步点火。
The calculated parameters of steady detonation wave front are compared with those of CJ theory, and the good agreements can be obtained.
稳定爆震波阵面参数与CJ理论结果进行了对比,两者符合得较好。
The numerical results agree well with experimental data and provide theoretical basis for engineering design of detonation wave igniter.
并与试验结果进行了对比分析,数值模拟结果和试验结果符合很好,为爆震波点火器的工程设计提供了理论依据。
Besides, all detonation tubes reached the speed of detonation wave when the local evaporator was employed to improve the fuel evaporation.
采用局部蒸发器改善燃油蒸发后,爆震管都达到了爆震波的传播速度。
The paper used the characteristics line method to calculate the one-dimensional detonation wave propagation process inside a detonation tube.
本文应用特征线法给出一维爆震波在爆震管内的传播过程的解析解。
The detonation wave resistance of multi-layer structures composed of Kevlar composites and amour steels was studied by using simulation test device.
利用防爆轰波模拟试验装置研究了由装甲钢和芳纶复合材料组成的不同复合结构对爆轰波的防护性能。
Correlating detonation wave propagation with the conjugate pairs appearing in micro-explosion and annihilating in expansion, the conjugate detonation model is established.
共轭对在微爆炸中产生并在膨胀中湮没,将此过程与爆轰波传播相关联,建立了共轭爆轰模型。
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。
With a high resolution ENO(Essentially Non oscillatory) scheme and a detailed chemical reaction model, one dimensional detonation wave structure of H 2 O 2 mixture was calculated.
采用高精度的ENO格式和基于基元化学反应的真实化学反应模型求解氢氧混合气体一维爆轰波的精细结构。
The ignition threshold of laser supported detonation wave (LSDW) can be determined based on the component variation of plasma in the laser absorption zone with laser power density.
根据激光吸收区等离子体组分与激光功率密度的关系判定激光支持爆轰波(LSDW)的点燃阈值。
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。
It shows that the boundary layer induced behind a 2 ATM 2h2 + O2, mixture detonation wave may undergo a transition from laminar to turbulent and then turn out a turbulent boundary layer.
值得指出的是,2大气压下2h_2 + O_2气体爆轰波后诱导引起的附面层可能经历着从层流向湍流的转捩,而后成为湍流附面层。
This paper introduces the experimental method of observing an oblique detonation wave standing in a laboratory reference frame with a shock tunnel, the experimental setup and primary results.
本文介绍了使用激波风洞观察相对实验室驻定的斜爆轰波的方法、实验装置和初步实验结果。
In conjugate detonation model, chemical reaction is initiated by the shock wave front, and the released energy makes the particles of explosion products move in different directions.
在共轭爆轰模型中,阵面激发化学反应释放出的能量,使得爆轰产物粒子朝不同的方向运动。
Under this critical condition, the cellular pattern, the velocity and maximum pressure along the wall and the wave evolution of marginal detonation were obtained.
在此临界条件下,获得了临界爆轰胞格结构、沿壁面的速度和峰值压力曲线及流场波系演变特征。
The damage area of cloud detonation shock wave increases linearly with the total energy of cloud detonation.
云爆冲击波的毁伤面积随固定云爆体积内总能量线性增加。
The damage area of cloud detonation shock wave increases linearly with the total energy of cloud detonation.
云爆冲击波的毁伤面积随固定云爆体积内总能量线性增加。
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