Hydrogen-Enriched Methane Flames in a Swirl Stabilized Combustor with Axial Air Injection

Master Thesis (2024)
Author(s)

V. De Lauso (TU Delft - Aerospace Engineering)

Contributor(s)

Ivan Langella – Mentor (TU Delft - Flight Performance and Propulsion)

Faculty
Aerospace Engineering
More Info
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Publication Year
2024
Language
English
Graduation Date
13-09-2024
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering | Flight Performance and Propulsion']
Faculty
Aerospace Engineering
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Abstract

This thesis explores the dynamics of hydrogen-enriched methane flames in a swirl-stabilized combustor with axial air injection, a configuration crucial for advancing low-emission combustion technologies. The study focuses on enhancing the understanding of flame behaviour under varying hydrogen enrichment levels, with particular attention to the effects of heat loss and strain on flame shape, mixing, and emissions. Utilizing computational methods, the research investigates key operating scenarios from the APPU project, refining thermal boundary predictions through an improved Heat Resistance Tuning approach. Additionally, it assesses the performance of a necessary flashback-prevention method, Axial Air Injection, quantifying its impact on mixing and flame shape, including their effects on temperature and pollutant formation, with varying results based on the level of hydrogen enrichment in the fuel. The results offer valuable insights that could inform control strategies for the stable and efficient operation of hydrogen-enriched combustion systems, supporting the development of fuel-flexible and environmentally sustainable propulsion technologies.

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