Some stratification exists in the spray produced by any liquid propellantinjector.
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。
2
Flow in injector passages of a variable thrust liquid propellant rocket engine was studied.
本文对变推力液体火箭发动机喷注器通道内介质流动进行求解。
3
The results of the calculation and the analysis of effects of combustion chamber pressure, mixture ratio, propellant injection temperature and injector type on the combustion processes are reported.