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Numerical Study on Secondary Jet Injection of Fluid for Thrust Vectoring in 2-D Supersonic Nozzle
2020
International Journal of Mechanical and Production Engineering Research and Development
Maneuvering of high speed aircraft is a challenging part during designing of the jet aircrafts in which various proposals had come with many solutions which includes the Secondary fluidic thrust vectoring. Here the study is performed to observe the flow variation by injecting the secondary fluid at eh exit of the nozzle. In supersonic nozzles due to injection of secondary liquid we observed shock and formation of these shocks are studied well. Fluidic thrust vectoring with the shock vector
doi:10.24247/ijmperdjun2020832
fatcat:a64u7zofafefzdlxkvwou4rwpu