Experimental and Numerical Studies of Secondary Injection in Nozzle Divergence for Thrust Augmentation
Sign Up to like & getrecommendations! Published in 2019 at "Journal of Applied Fluid Mechanics"
DOI: 10.29252/jafm.12.05.29842
Abstract: Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is an innovative extension of after burners. This technique finds application in single stage to orbit propulsion devices, where the… read more here.
Keywords: numerical studies; thrust augmentation; injection; augmentation ... See more keywords