Direct numerical simulation of a high-pressure hydrogen micromix combustor: flame structure and stabilisation mechanism
Thomas L. Howarth, Mark A. Picciani, Edward S. Richardson, Marcus S., Day, Andrew J. Aspden

TL;DR
This study uses direct numerical simulation to analyze the flame structure and stabilization mechanisms in a high-pressure hydrogen micromix combustor, revealing ignition-driven stabilization and detailed flame zones.
Contribution
It provides a detailed numerical analysis of flame stabilization in a hydrogen micromix combustor, highlighting ignition events and turbulence effects, which are novel insights for high-pressure combustion.
Findings
Core flame burns over 85% of fuel
Ignition events driven by shear-induced vortices
Stabilization due to turbulent mixing and ignition
Abstract
A high-pressure hydrogen micromix combustor has been investigated using direct numerical simulation with detailed chemistry to examine the flame structure and stabilisation mechanism. The configuration of the combustor was based on the design by Schefer [1], using numerical periodicity to mimic a large square array. A precursor simulation of an opposed jet-in-crossflow was first conducted to generate appropriate partially-premixed inflow boundary conditions for the subsequent reacting simulation. The resulting flame can be described as a predominantly-lean inhomogeneously-premixed lifted jet flame. Five main zones were identified: a jet mixing region, a core flame, a peripheral flame, a recirculation zone, and combustion products. The core flame, situated over the jet mixing region, was found to burn as a thin reaction front, responsible for over 85% of the total fuel consumption. The…
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Taxonomy
TopicsCombustion and flame dynamics · Combustion and Detonation Processes · Advanced Combustion Engine Technologies
