| 1. | Rapid reactions between liquid propellants can lead to inefficient mixing .
液体推进剂之间的迅速反应可能导致混合不良。 |
| 2. | It is reasonable that this result should be generally applicable also to liquid-propellant rockets .
这个结果通常也应适用于液体推进剂火箭。 |
| 3. | Some stratification exists in the spray produced by any liquid propellant injector .
由任何液体推进剂喷注器所产生的喷雾都存在某些成层现象。 |
| 4. | Liquid propellant combustion processes are quite complicated and defy precise analytical description .
液体推进剂燃烧过程是相当复杂的，很难对其进行严谨的分析描述。 |
| 5. | The application of a pressure difference across an injector does not cause an immediate velocity response of the liquid propellant .
经过喷注器的压降发生变化时并不马上引起液体推进剂速度变化。 |
| 6. | The time lag can be envisioned as the time required for the liquid propellants to travel from the injector to an effective combustion "front. "
可以把迟滞想象为液体推进剂从喷注器运行到有效燃烧“锋”所需的时间。 |
| 7. | To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood .
为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。 |
| 8. | When liquid propellants are used the fuel and oxidize are fed under pressure to one or more combustion chambers and expanded to atmosphere through convergent-divergent nozzles .
当使用液体推进剂时，在压力作用下，燃料和氧化剂输送到一个或几个燃烧室中，并通过收敛-打散喷管，排到大气中。 |
| 9. | An analysis of shockwave superpressure for liquid propellant explosion
液体推进剂爆炸实验冲击波超压分析 |
| 10. | Liquid propellant rocket
液体推进剂火箭 |
