Lagrangian modelling of turbulent spray combustion under liquid rocket engine conditions

Lagrangian modelling of turbulent spray combustion under liquid rocket engine conditions

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Article ID: iaor20141168
Volume: 94
Issue: 1
Start Page Number: 184
End Page Number: 197
Publication Date: Jan 2014
Journal: Acta Astronautica
Authors: , ,
Keywords: modelling, Lagrangian methods, aerospace
Abstract:

  • A robust computational model is considered to describe LOx–GH2 combustion.
  • The combustion model includes the influence of vaporization‐induced fluctuations.
  • Their consideration is essential to describe composition statistics and flame shape.
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