In order to investigate the influence of characteristics parameters on detonation wave in a two - phase pulse detonation engine model . the peak detonation pressures and average velocities of two - phase pulsed detonation wave produced by pde model using gasoline as fuel and air as oxidizer under various ignition frequencies and various mixture ratios are measured systematically , and the relations influencing them are analyzed 为了探索气-液两相脉冲爆震发动机模型内特征参数对产生爆震波的影响规律，系统地测试了以汽油为燃料、以空气为氧化剂的气-液两相脉冲爆震发动机模型在不同点火频率及不同余气系数下爆震波的峰值压力以及平均爆震波速，并对其变化进行了分析。
Then using kerosene as fuel , oxygen and compressed air as oxidizers , proof - of - principle experiments of pdre were successfully conducted the results show that the measured detonation wave pressures are close to theoretical values it also indicate that using kerosene as the fuel of pdre is feasible 采用航空煤油为燃料，氧气和压缩空气为氧化剂，分别进行了两相脉冲爆震火箭发动机原理性试验，所测得的爆震波压力接近充分发展的理想爆震波压力，说明采用煤油作为脉冲爆震火箭发动机的燃料是可行的。
