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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, an experimental study was carried out on three annular slots of different area ratios, using hydrogen as fuel and air as oxidant. Based on the high frequency pressure signal, the influence 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 wave propagates in a double-wave colliding mode, and the peak pressure is in the range of 0.3-0.9MPa. When the area ratio is 0.16, the detonation wave propagates in single wave mode, and the pressure peak is around 2.0MPa. When the area ratio is 0.32, the detonation wave propagates in a single-wave/double-wave coexistence mode, and the peak pressure fluctuation ranges from 0.4 to 3.0 MPa. When the area ratio is 0.08, the detonation wave self-sustaining propagation stability is strong, but the detonation wave stability is weak when the area ratio is too large or too small. Therefore, the area ratio of the annular slot has a great influence on the mixing effect of hydrogen and air, which consequently impacts the detonation stability of the continuous rotating detonation engine.
机译:为了研究连续旋转爆震发动机的爆震稳定性,实验研究是在不同面积比的三个环形槽进行,使用氢作为燃料和空气作为氧化剂。基于所述高频压力信号,在爆轰参数稳定性环状槽面积比的影响进行了分析。实验结果表明,当面积比为0.08,在双波碰撞模式的爆轰波传播,峰值压力在0.3-0.9MPa范围内。当面积比为0.16,爆轰波在单波模式传播,压力峰值为约2.0MPa的。当面积比为0.32,在一个单一的波/双波共存模式爆轰波传播,并且峰值压力波动范围为0.4至3.0MPa。当面积比为0.08,爆轰波自持传播稳定性强,但爆轰波稳定性较弱当面积比过大或过小。因此,环状槽的面积比对氢气和空气的混合效果,有很大的影响,其结果影响到连续旋转的爆震发动机的爆震的稳定。

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