| 1. | Front of the detonation wave
爆震波波前 |
| 2. | Numerical simulation on propagation process of detonation wave in detonation combustion chamber
爆震波在爆震燃烧室内传播过程的数值模拟 |
| 3. | A study of the law of mixture pressure influence on the characteristic parameters of detonation wave
混合气压力对爆震波特征参数的影响规律 |
| 4. | Element potential approach and its application to calculation of characteristic parameters of detonation wave
元素势法在爆震波特征参数计算中的应用 |
| 5. | Effect of initial pressure on characteristic parameters of detonation wave in pde pulse detonation engine
混合气体燃烧中压力对爆震波特性参数影响研究 |
| 6. | Effects of parameters of turbulence generator on the detonation wave in air - breathing gasoline - air pulse detonation engine
空气脉冲爆震发动机爆震波压力的影响 |
| 7. | 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
摘要实验研究了爆轰波在声学吸收段下游发生的再恢复过程。 |
| 8. | The three - dimensional ( 3d ) euler equations are applied to the study of numerical simulation of chemical non - equilibrium oblique detonation wave standing on an accelerating projectile with attack angle
摘要采用三维非定常化学反应控制方程组对驻定在带攻角高速飞行弹丸上的斜爆轰波流场进行了数值模拟。 |
| 9. | 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。 |
| 10. | 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。 |
