By applying the obtained thrustaugmentation mechanism, an improved RBCC configuration was proposed.
应用研究获得的推力增强机理提出了实验样机构型的改进方案。
2
It is in the first time in domestic RBCC researches that the RBCC configuration with relatively higher thrustaugmentation in ejecting mode is obtained.
Lab tests showed that 55% thrustaugmentation should be expected; however, differences in the scaled-up system dropped augmentation levels to 19% for the wing and a mere 6% in the canard.