Computational investigation of secondary flow thrust vector control technology used in a convergent-divergentnozzle;
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
2
The nozzle was entirely blackened, with the hottest region being where the throat meets the divergent section .
喷嘴是完全发黑的，与最热门的地区正在那里喉咙会见不同的区段。
3
There are particles on whole cross section of nozzledivergent section and this fact shows that there is no"no particles zone"in nozzledivergent section.