How "mixing" affects propagation and structure of intensely turbulent, lean, hydrogen-air premixed flames
Yuvraj (1), Hong G. Im (2), Swetaprovo Chaudhuri (1) ((1) Institute, for Aerospace Studies, University of Toronto, Toronto, Canada, (2) Clean, Combustion Research Center, King Abdullah University of Science and, Technology, Thuwal, Saudi Arabia)

TL;DR
This study investigates how turbulence influences the structure and propagation speed of lean hydrogen-air premixed flames using DNS, revealing effects of differential diffusion, curvature, and flame interactions on flame speed and structure.
Contribution
It provides new insights into the variation of flame displacement speeds and structure in turbulent hydrogen flames, especially near zero-curvature regions, through detailed DNS analysis.
Findings
Enhanced local flame speed due to differential diffusion in low Le cases.
Reversal of flame speed gradient caused by flame-flame interactions.
Statistical analysis of flame structure variations at zero-curvature regions.
Abstract
Understanding how intrinsically fast hydrogen-air premixed flames can be rendered much faster in turbulence is crucial for systematically developing hydrogen-based gas turbines and spark ignition engines. Here, we present fundamental insights into the variation of flame displacement speeds by investigating how the disrupted flame structure affects speed and vice-versa. Three DNS cases of lean hydrogen-air mixtures with from 0.5 to 1 and from 100 to 1000 are analyzed. Suitable comparisons are made with the closest canonical laminar flame configurations at same mixture conditions and their suitability and limitations in expounding turbulent flame properties are elucidated. Since near zero-curvature surface locations are most probable and representative of the average flame geometry in such large flames, this study focuses on the statistical variation of flame displacement…
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Taxonomy
TopicsCombustion and flame dynamics · Combustion and Detonation Processes · Rocket and propulsion systems research
