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Tag Archives: Combustion Performance

Numerical Study of Reactive Flow dynamics in a Hydrogen-fueled Direct-Connect Scramjet Combustor depending on Number of Injector

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusJune 7, 2024

Seung-Min JEONG, Jae-Eun KIM, Jeong-Yeol CHOI

DOI Number: 10.60853/07a4-dk14

Conference number: HiSST-2024-00350

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