Enhancement of chemical heat release in a generic scramjet combustor using plasma injection modules-Reference-Cited by-同舟云学术

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Enhancement of chemical heat release in a generic scramjet combustor using plasma injection modules

Published:2024 Issue:1-4 Volume:40 Page:105664
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Braun Erik L.^ORCID,Hammack Stephen D.^ORCID,Ombrello Timothy M.,Lax Philip,Leonov Sergey B.^ORCID

Funder

Air Force Research Laboratory

Publisher

Elsevier BV

Reference19 articles.

1. Review of combustion stabilization for hypersonic airbreathing propulsion;Liu;Prog. Aerosp. Sci.,2020

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

3. Plasma-assisted ignition and combustion;Starikovskiy;Prog. Energy Combust. Sci.,2013

4. Plasma assisted combustion: dynamics and chemistry;Ju;Prog. Energy Combust. Sci.,2015

5. The use of a plasma jet for flame stabilization and promotion of combustion in supersonic air flows;Kimura;Combust. Flame,1981

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