Studies on the critical flame radius and minimum ignition energy for spherical flame initiation

Zheng Chen, Michael P. Burke, Yiguang Ju

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Abstract

Flame initiation from an ignition kernel is studied theoretically and numerically for different fuel (hydrogen, methane, and propane)/oxygen/helium/ argon mixtures by using a spherical flame. The objectives are to find the controlling length scale for flame initiation in a quiescent mixture and to reveal its relationship with the minimum ignition energy. The results show that, different from the flame thickness or flame ball radius, there is a critical flame radius that controls flame initiation. The minimum ignition energy for successful flame initiation is found to be proportional to the volume defined by the critical flame radius. Furthermore, the preferential diffusion between heat and mass (Lewis number effect) is found to play an important role in affecting the critical flame radius and flame initiation. It is shown that the critical flame radius and the minimum ignition energy increase significantly with the increase of Lewis number. Therefore, for large molecular hydrocarbon fuels with low mass diffusivity, significantly larger ignition energy is needed to initiate successfully a self-sustained propagating premixed flame.

Original languageEnglish (US)
Title of host publication47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
StatePublished - 2009
Event47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States
Duration: Jan 5 2009Jan 8 2009

Publication series

Name47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Other

Other47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Country/TerritoryUnited States
CityOrlando, FL
Period1/5/091/8/09

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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