Enhancement of blowout limit in a Mach 2.92 cavity-based scramjet combustor by a gliding arc discharge-Reference-Cited by-同舟云学术

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Enhancement of blowout limit in a Mach 2.92 cavity-based scramjet combustor by a gliding arc discharge

Published:2022-09 Issue: Volume: Page:
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Tian Yifu,Zhu Jiajian,Sun Mingbo,Wang Hongbo,Huang Yuhui,Feng Rong,Yan Bo,Sun Yongchao,Cai Zun

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference21 articles.

1. Cavity flame-holders for ignition and flame stabilization in scramjets: an overview;Ben-Yakar;J. Propul. Power,2001

2. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder;Micka;Proc. Combust. Inst.,2009

3. Correlation and analysis of blowout limits of flames in high-speed airflows;Driscoll;J. Propul. Power,2005

4. Lean blowoff behavior of cavity-stabilized flames in a supersonic combustor;Wang;Aerosp. Sci. Technol.,2021

5. Characteristics of cavity-stabilized flames in a supersonic flow;Rasmussen;J. Propul. Power,2005

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