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
A new propulsion concept of 2 D C D vectoring nozzle was proposed, which had a convergent duct shaped by spheric surface and a divergent one with rectangular transverse section.