Reactive Flow Dynamics of Low-Frequency Instability in a Scramjet Combustor

This study numerically investigated the combustion instability and characteristics of a laboratory-scale gaseous hydrogen-fueled scramjet combustor. For this purpose, a numerical simulation with an improved detached eddy simulation and a detailed hydrogen/oxygen reaction mechanism was performed. The...

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Hlavní autoři:	Seung-Min Jeong, Hyung-Seok Han, Bu-Kyeng Sung, Wiedae Kim, Jeong-Yeol Choi
Médium:	Artigo
Jazyk:	Inglês
Vydáno:	MDPI AG 2023-10-01
Edice:	Aerospace
Témata:	scramjet engine supersonic combustion low-frequency instability upstream-traveling shock wave combustion mode
On-line přístup:	https://www.mdpi.com/2226-4310/10/11/932
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