Large-eddy simulation of a supersonic lifted jet flame: Analysis of the turbulent flame base

  title={Large-eddy simulation of a supersonic lifted jet flame: Analysis of the turbulent flame base},
  author={Lisa Bouheraoua and Pascale Domingo and Guillaume Ribert},
  journal={Combustion and Flame},

Stabilization mechanisms of lifted flames in a supersonic stepped-wall jet combustor

Flame stabilization is the key to extending scramjets to hypersonic speeds; accordingly, this topic has attracted much attention in theoretical research and engineering design. This study performed

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The facilitation of a stable combustion process is of utmost importance for the realizability and performance of hypersonic propulsion systems. To elucidate the turbulent combustion characteristics,

Analysis of combustion modes in a cavity based scramjet



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The simulation of supersonic combustion requires finite‐rate chemistry because chemical and fluid mechanical time scales may be of the same order of magnitude. The size of the chosen reaction

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A chemical explosive mode analysis (CEMA) was developed as a new diagnostic to identify flame and ignition structure in complex flows. CEMA was then used to analyse the near-field structure of the

Finite Rate Chemistry Large-Eddy Simulation of Self-Ignition in a Supersonic Combustion Ramjet

In this study, large-eddy simulation is used to analyze supersonic flow, mixing, and combustion in a supersonic combustor equipped with a two-stage fuel injector strut. The present study focuses on