Effect of combustion chamber diameter size on scramjet rotating detonation under high Mach number flow conditions

Effect of combustion chamber diameter size on scramjet rotating detonation under high Mach number flow conditions

This study conducted 3D numerical simulations to investigate the impact of combustion chamber diameter on the combustion characteristics of liquid kerosene scramjet rotating detonation under high Mach number flow conditions (Ma6/28 km). After ignition, a local hotspot near the contact surface betwee...

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Bibliographic Details
Main Authors: Chen Shu, Wei Lin, Yiheng Tong, Siyin Zhou, Chenglong Yan, Yuchao Gao
Format: Article
Language:English
Published: AIP Publishing LLC 2023-10-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/5.0170019

Internet

http://dx.doi.org/10.1063/5.0170019

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