Combustion Modes and Unsteady Characteristics during the Condition Transition of a Scramjet Combustor

To investigate the combustion modes and unsteady characteristics during the condition transition of a scramjet combustor, a series of experiments were carried out under the condition of Mach 2.52 supersonic incoming flow, the corresponding stagnation pressure and temperature of which were 1.6 MPa an...

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Bibliographic Details
Published in:Energies
Main Authors: Dongpeng Jia, Yu Pan, Ning Wang, Chaoyang Liu, Kai Yang
Format: Article
Language:English
Published: MDPI AG 2021-04-01
Subjects:
condition transition
flame stabilization
blowout
flame oscillation
unsteady combustion
Online Access:https://www.mdpi.com/1996-1073/14/9/2522

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