Numerical Investigation on Pylon and Flush Wall Injection in Cold Coaxial Jets

The dual combustion ramjet (DCR) engine is considered one of the promising engines for the hypersonic missile propulsion system. This paper reveals the non-reacting flow characteristics of the DCR engine with the influence of pylon and wall injections in coaxial jets using numerical investigation. T...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2021-04, Vol.1128 (1), p.12035
Hauptverfasser:	Sarathkumar Sebastin, J., Jeyakumar, S., Karthik, K., Sivakumar, R.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Combustion chambers Compressibility Computational fluid dynamics Flow characteristics Gas generators Gaseous fuels Jets Missile propulsion Nozzles Numerical analysis Pressure loss Propulsion systems Reacting flow Reynolds averaged Navier-Stokes method Shock waves Spatial distribution Supersonic flow Turbulence models
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