Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 11 September 2024
Issue publication date: 25 September 2024
Abstract
Purpose
This study aims to numerically analyse a full-scale burner across a wide range of operating pressure conditions and determine the effect of swirl velocity on flame stabilization, flame holding and combustion performance.
Design/methodology/approach
This study uses a numerical analysis approach to investigate a three-dimensional full-scale burner. Modified governing equations are used to determine the effect of swirl velocity on flame stabilization and flame holding. The GR-Mech 3.0 chemical reaction mechanism is used to predict the combustion process. To validate the model, a grid independence study is performed.
Findings
The study reveals that swirl velocity enhances flame stability, resulting in better combustion rates. As the swirl velocity increases, higher flame temperatures are observed due to high convective heat recirculation. The heat transfer coefficient and high radiative extinction coefficient are found to vary based on fuel swirl velocity. The mass fraction of CH4 and CO emphasizes the role of swirl velocity on flame structure. Increasing velocity potentially improves combustion by delaying the process, leading to better combustion and lower emissions.
Originality/value
The findings of this study contribute to the understanding of swirl-stabilized combustion and can guide the development of advanced combustion technologies, making it a valuable addition to the existing combustion field.
Keywords
Acknowledgements
Corrigendum: It has come to the attention of the publisher that the article Paramasivam, P., Obaid, S.A. and Balasubramanian, A. (2024), “Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design”, Aircraft Engineering and Aerospace Technology, Vol. ahead-of-print No. ahead-of-print. https://doi.org/10.1108/AEAT-05-2024-0137, displays the acknowledgement incorrectly. This error was introduced during the submission process. “This project was supported by researchers supporting Project number (RSP2024R315), King Saud University, Riyadh, Saudi Arabia” has been corrected to “This project was supported by Researchers Supporting Project number (RSP2025R315) King Saud University, Riyadh, Saudi Arabia”. The authors sincerely apologise for this error and for any misunderstanding.
This project was supported by Researchers Supporting Project number (RSP2025R315) King Saud University, Riyadh, Saudi Arabia.
Funding: There are no funding bodies/agencies involved in this research work and the authors solely contribute to it.
Competing interests: The authors declare that they have no competing interests.
Availability of data and materials: The data is available within the manuscript.
Author contribution: PP: Conceptualization, methodology, data curation, project administration, writing – original draft; SAO: Writing – review and editing, resources, validation and AB: Supervision, software.
Citation
Paramasivam, P., Obaid, S.A. and Balasubramanian, A. (2024), "Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design", Aircraft Engineering and Aerospace Technology, Vol. 96 No. 8, pp. 1045-1052. https://doi.org/10.1108/AEAT-05-2024-0137
Publisher
:Emerald Publishing Limited
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