Theory article

Effects of oxygen concentration of oxidizer flow on laminar diffusion flame established over liquid fuel beds at microgravity

  • Received: 27 November 2023 Revised: 19 February 2024 Accepted: 28 February 2024 Published: 12 March 2024
  • The effects of oxygen concentration in oxidizer flow with a low speed of 0.1–0.3 m/s on a co-current flame spread over a thin liquid fuel bed at microgravity is numerically studied. The soot model is based on the Laminar Smoke Point (LSP) concept, which was used to reproduce the behaviour of a non-premixed, heavily sooting laminar flame. The results including flame patterns, soot emissions, temperature, and liquid burning rate are examined. Pyrolysis rate of liquid fuel significantly increases by increasing forced flow velocity and oxygen concentration, favouring flame length and soot formation. The flame behaviour at very low strain rates depends on both radiative heat loss and combustion efficiency, which are affected by oxygen concentration. The reactive boundary layer is significantly lifted along the pyrolysis surface due to lack of oxygen in the growing boundary layer, and the 3D effects are of importance due to thermal expansion. The ratio between the flame stand-off distance and the boundary layer thickness converges toward unity, however, the soot resides within the boundary layer. Compared to a heptane flame, a dodecane flame has lower pyrolysis rate and more effective oxygen transport ensures intensive combustion. A high oxidizer flow velocity results in a longer flame, and a reduction in flame standoff distance from the flat plate.

    Citation: Hui Ying WANG, Némo DECAMPS. Effects of oxygen concentration of oxidizer flow on laminar diffusion flame established over liquid fuel beds at microgravity[J]. Metascience in Aerospace, 2024, 1(2): 159-184. doi: 10.3934/mina.2024007

    Related Papers:

  • The effects of oxygen concentration in oxidizer flow with a low speed of 0.1–0.3 m/s on a co-current flame spread over a thin liquid fuel bed at microgravity is numerically studied. The soot model is based on the Laminar Smoke Point (LSP) concept, which was used to reproduce the behaviour of a non-premixed, heavily sooting laminar flame. The results including flame patterns, soot emissions, temperature, and liquid burning rate are examined. Pyrolysis rate of liquid fuel significantly increases by increasing forced flow velocity and oxygen concentration, favouring flame length and soot formation. The flame behaviour at very low strain rates depends on both radiative heat loss and combustion efficiency, which are affected by oxygen concentration. The reactive boundary layer is significantly lifted along the pyrolysis surface due to lack of oxygen in the growing boundary layer, and the 3D effects are of importance due to thermal expansion. The ratio between the flame stand-off distance and the boundary layer thickness converges toward unity, however, the soot resides within the boundary layer. Compared to a heptane flame, a dodecane flame has lower pyrolysis rate and more effective oxygen transport ensures intensive combustion. A high oxidizer flow velocity results in a longer flame, and a reduction in flame standoff distance from the flat plate.



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