Experimental and Numerical Study of the Flammability Limits in a CH<sub>4</sub>/O<sub>2</sub> Torch Ignition System

The current work is devoted to studying combustion initiation inside the methane-oxygen torch igniter for a hybrid rocket motor. The ignition system can generate a wide range of power and oxidizer-to-fuel ratios. It has a self-cooled vortex combustion chamber with one fuel jet injector and one circu...

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Bibliographic Details
Main Authors: Olexiy Shynkarenko, Domenico Simone, Jungpyo Lee, Artur E. M. Bertoldi
Format: Article
Language:English
Published: MDPI AG 2022-05-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/15/11/3857