Ignition and combustion enhancement in a cavity-based supersonic combustor by a multi-channel gliding arc plasma-Reference-Cited by-同舟云学术

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Ignition and combustion enhancement in a cavity-based supersonic combustor by a multi-channel gliding arc plasma

Published:2021-01 Issue: Volume:120 Page:110248
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Feng Rong,Huang Yuhui,Zhu Jiajian,Wang Zhenguo,Sun Mingbo,Wang Hongbo,Cai Zun

Funder

Foundation of Innovation-oriented Province Construction of Hunan

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference52 articles.

1. Experimental study of oscillations in a scramjet combustor with cavity flameholders;Wang;Exp. Therm. Fluid Sci.,2013

2. Cavity-based flameholding for chemically-reacting supersonic flows;Barnes;Prog. Aerosp. Sci.,2015

3. On shock train interaction with cavity oscillations in a confined supersonic flow;Kumar;Exp. Therm. Fluid Sci.,2018

4. Research on supersonic combustion;Billig;J. Propul. Power,1993

5. Review of cavity ignition in supersonic flows;Cai;Acta Astronaut.,2019

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