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EXPERIMENTAL STUDY ON CONTINUOUS ROTATING DETONATION ENGINE

机译:连续旋转爆轰发动机的实验研究

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In order to study the detonation stability of continuous rotating detonation engine, anexperimental study was carried out on three annular slots of different area ratios, usinghydrogen as fuel and air as oxidant. Based on the high frequency pressure signal, theinfluence of the annular slot area ratio on the detonation parameter stability was analyzed.The experimental results show that when the area ratio is 0.08, the detonation wavepropagates in a double-wave colliding mode, and the peak pressure is in the range of0.3-0.9MPa. When the area ratio is 0.16, the detonation wave propagates in single wavemode, and the pressure peak is around 2.0MPa. When the area ratio is 0.32, the detonationwave propagates in a single-wave/double-wave coexistence mode, and the peak pressurefluctuation ranges from 0.4 to 3.0 MPa. When the area ratio is 0.08, the detonation waveself-sustaining propagation stability is strong, but the detonation wave stability is weakwhen the area ratio is too large or too small. Therefore, the area ratio of the annular slot hasa great influence on the mixing effect of hydrogen and air, which consequently impacts thedetonation stability of the continuous rotating detonation engine.
机译:为了研究连续旋转爆炸发动机的爆震稳定性,在不同面积比的三个环形槽上进行实验研究,使用氢气作为燃料和空气作为氧化剂。基于高频压力信号,分析了环形槽面积比对爆轰参数稳定性的影响。实验结果表明,当面积比为0.08时,爆炸波以双波碰撞模式传播,峰值压力在于0.3-0.9mpa。当面积比为0.16时,爆炸波以单波传播模式,压力峰值约为2.0MPa。当面积比为0.32时,爆炸波以单波/双波共存模式和峰值压力传播波动范围为0.4至3.0 MPa。当面积比为0.08时,爆炸波自我维持的传播稳定性强,但爆炸波稳定性较弱当面积比太大或太小时。因此,环形槽的面积比具有对氢气和空气的混合效果产生了很大影响,从而影响连续旋转爆轰发动机的爆震稳定性。

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