Outflow Boundary Conditions for Turbine-Integrated Rotating Detonation Combustors

This study examines outflow boundary conditions (BCs) in computational fluid dynamics (CFD) simulations of a transition duct with and without guide vanes that converts supersonic flow exiting a rotating detonation combustor (RDC) to subsonic flow to drive a turbine. Since the flow exiting the transi...

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Principais autores:	Tsung-Ming Hsieh, K. Mark Bryden, Richard P. Dalton, John Crane, Tom I-P. Shih
Format:	Artigo
Jezik:	Inglês
Izdano:	MDPI AG 2025-11-01
Serija:	Applied Sciences
Teme:	outflow boundary conditions nonreflecting boundary conditions rotating detonation combustors rotating detonation engines gas turbines
Online dostop:	https://www.mdpi.com/2076-3417/15/22/11922
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