Stationary ethylene–air edge flames in a wedge-shaped region at low and high strain rates

Ben Shields, Jonathan B. Freund, Carlos Pantano

Research output: Contribution to journalArticlepeer-review

Abstract

Edge flames are a canonical two-dimensional flame structure appearing in lifted jet flames and in the growth and repair of flame holes in nonpremixed turbulent combustion. Computational studies of edge flames with hydrodynamic-coupling at high strains are difficult owing to difficulties defining a stationary state. A wedge-shaped counterflow configuration is here used to provide control over the position of the edge flame, and allowing access to stationary, hydrodynamically-coupled retreating flames (at low and high strains). ethylene–air edge flames are established in the resulting non-uniformly strained counterflow, with combustion modeled using a skeletal reduction of the USC Mech II. The details of the ethylene–air edge flame are discussed, and comparisons are made between stoichiometric, fuel-lean, and fuel-rich compositions. Mixture-fraction-based coordinates local to the flame front are developed and analysed for a range of edge-flame speeds and compositions. A strain-rate parameter is described that admits a speed-strain relationship that is insensitive to the mixture stoichiometry, and a model for retreating flame speeds at high strain rates is discussed.

Original languageEnglish (US)
Pages (from-to)1039-1063
Number of pages25
JournalCombustion Theory and Modelling
Volume25
Issue number6
DOIs
StatePublished - 2021

Keywords

  • detailed chemistry
  • edge flame
  • eigenvalue problem
  • ethylene
  • flame speed

ASJC Scopus subject areas

  • General Chemistry
  • General Chemical Engineering
  • Modeling and Simulation
  • Fuel Technology
  • Energy Engineering and Power Technology
  • General Physics and Astronomy

Fingerprint

Dive into the research topics of 'Stationary ethylene–air edge flames in a wedge-shaped region at low and high strain rates'. Together they form a unique fingerprint.

Cite this