An Experimental on Cellular Instability and Laminar Burning Velocity of SNG Fuel

SNG 연료의 셀 불안정성 및 층류연소속도에 관한 실험적 연구

  • 김동찬 (순천대학교 우주항공공학전공) ;
  • 조준익 (쌍용자동차 기술연구소) ;
  • 이기만 (순천대학교 기계우주항공공학부)
  • Published : 2015.12.10

Abstract

This article describes a cellular instability and laminar burning velocity of simulated synthetic natural gas(SNG) including 3% hydrogen. In this study, experimental apparatus is employed using cylindrical bomb combustor, and investigation is carried out with high speed camera and Schlieren system. The cellular instability is caused by the buoyancy, hydrodynamic instability. Unstretched burning velocity can be determined by extrapolated stretch rate of zero point from measured results. These results were also compared with numerical calculation by Chemkin package with GRI 3.0, USC-II, WANG, C3 Fuel mechanism. As an experimental conditions, equivalence ratios was adjusted from 0.8 to 1.3. From results of this work, the one was found that the cellular instability has occurred by effect of thermal expansion rate and flame thickness. As the other results, unstretched laminar burning velocity was best coincided with GRI 3.0 mechanism.

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