DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)

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Veröffentlicht in:	AIAA Propulsion and Energy Forum (2021 : Online) Gas turbine engines
1. Verfasser:	Ramesh, Rahul (VerfasserIn)
Weitere Verfasser:	Obidov, Sanjar (VerfasserIn), Paredes, Juan (VerfasserIn), Bernstein, Dennis S. (VerfasserIn), Gamba, Mirko (VerfasserIn)
Format:	UnknownFormat
Sprache:	eng
Veröffentlicht:	2021
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