Hybrid Kerosene-Hydrogen Flames Modeling and Topology Analysis

From a Computational Perspective

Master Thesis (2026)
Author(s)

D.T.A. Tavernier (TU Delft - Aerospace Engineering)

Contributor(s)

Francesca De Domenico – Mentor (TU Delft - Aerospace Engineering)

Lorenzo Palanti – Mentor (Ergon Research SRL)

Faculty
Aerospace Engineering
More Info
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Publication Year
2026
Language
English
Coordinates
11.2384, 43.7915
Graduation Date
20-07-2026
Awarding Institution
Delft University of Technology
Project
HOPE (Hydrogen Optimized multi-fuel Propulsion system for clean and silEnt aircraft)
Programme
Aerospace Engineering, Aerodynamics
Sponsors
Ergon Research SRL
Faculty
Aerospace Engineering
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Abstract

This study, conducted within the HOPE (Hydrogen Optimized multi-fuel Propulsion system for clean and silEnt aircraft) project, examines how kerosene-hydrogen fuel blends affect flame topology in a multi-fuel combustor designed to advance hydrogen powered aviation. High-fidelity Stress-Blended Eddy Simulations were performed to reproduce experimental testing conducted at the Delft University Sustainable Propulsion Lab, and results were compared against available experimental data to assess the flame topology across pure hydrogen, pure kerosene, and multi-fuel cases. Additionally, lower-fidelity simulations were used to evaluate combustor performance under limiting engine operating conditions, specifically a hydrogen-only take-off scenario.

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