Eulerian Stochastic Field method with FGM tabulation

for Partially Premixed Hydrogen Flames

Master thesis (2024)

Authors

V.H. Vloeberghs Aerospace Engineering

Contributors

I. Langella Flight Performance and Propulsion - Aerospace Engineering (supervisor 1)
D.J.E.M. Roekaerts Fluid Mechanics - Mechanical, Maritime and Materials Engineering (supervisor 2)
Faculty
Aerospace Engineering
Copyright: © 2024 Victor Vloeberghs
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Published Date

01-02-2024

Language

English

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Faculty

Aerospace Engineering

Abstract

This thesis introduces a newly-developed turbulent combustion model, as a next step towards modelling hydrogen combustion in aircraft engines. The proposed model (FGM-ESF) merges the Flamelet Generated Manifold approach's tabulated chemistry with the Eulerian Stochastic Field method's statistical treatment of flame-turbulence interactions at the subgrid scales, which are not resolved in LES. This hybrid model excels in managing complex combustor dynamics, high turbulence, and both premixed and non-premixed combustion modes, all while maintaining computational efficiency. Validated with a lifted turbulent H2/N2 jet flame in vitiated coflow, reflecting typical combustor conditions, the FGM-ESF model produces accurate predictions of mean velocity, temperature, and mixture in close agreement with the experiments. Comparatively, its performance matches the more costly, fully transported chemistry ESF model, showing limited sensitivity to the number of stochastic fields. The balance between computational efficiency and precision in the FGM-ESF model highlights its importance in the advancement of hydrogen-powered aircraft engines.