Unsteady Oblique Detonation Waves in a Tunnel Induced by Inflow Mach Number Variation

Oblique detonation waves (ODWs) have been investigated widely aiming at facilitating their application in hypersonic engines. However, there is a lack of research on unsteady ODWs which are unavoidable in the hypersonic air-breathing scenario. In this study, unsteady ODWs triggered by the variation...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Shuzhen Niu, Pengfei Yang, Kuanliang Wang, Honghui Teng
Format:	Article
Language:	English
Published:	MDPI AG 2023-03-01
Subjects:	oblique detonation wave hypersonic flow unsteady Mach stem recirculation zone
Online Access:	https://www.mdpi.com/2226-4310/10/4/330