Direct numerical simulation of a high-pressure hydrogen micromix combustor: Flame structure and stabilisation mechanism-Reference-Cited by-同舟云学术

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Direct numerical simulation of a high-pressure hydrogen micromix combustor: Flame structure and stabilisation mechanism

Published:2024-07 Issue: Volume:265 Page:113504
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Howarth T.L.^ORCID,Picciani M.A.,Richardson E.S.,Day M.S.,Aspden A.J.^ORCID

Publisher

Elsevier BV

Reference52 articles.

1. Evaluation of NASA Lean Premixed Hydrogen Burner;Schefer,2003

2. An overview on dry low NOx micromix combustor development for hydrogen-rich gas turbine applications;Funke;Int. J. Hydrog. Energy,2019

3. 30 Years of dry-low-NOx micromix combustor research for hydrogen-rich fuels - an overview of past and present activities;Funke;J. Eng. Gas Turbines Power,2021

4. Experimental and numerical investigations of the dry-low-NOx hydrogen micromix combustion chamber of an industrial gas turbine;Haj Ayed;Propulsion Power Res.,2015

5. Numerical and experimental evaluation of a dual-fuel dry- low-NOx micromix combustor for industrial gas turbine applications;Funke;J. Thermal Sci. Eng. Appl.,2019

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