한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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Parallel Numerical Simulation of Shear Coaxial $LOX/GH_2$ Jet Flame in Rocket Engine Combustor

  • Matsuyama S. (Institute of Aerospace Technology, Japan Aerospace Exploration Agancy (JAXA)) ;
  • Shinjo J. (Institute of Aerospace Technology, Japan Aerospace Exploration Agancy (JAXA)) ;
  • Mizobuchi Y. (Institute of Aerospace Technology, Japan Aerospace Exploration Agancy (JAXA)) ;
  • Ogawa S. (Institute of Aerospace Technology, Japan Aerospace Exploration Agancy (JAXA))
  • Published : 2006.05.01
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Abstract

An axisymmetric simulation with detailed chemistry and fine resolution mesh is conducted for the $LOX/GH_2$ jet flame in rocket engine combustor. A preliminary result is shown for a single shear coaxial injector element. The fundamental features of the $LOX/GH_2$ coaxial jet flame is explored by the analysis of simulated flame.

Keywords