Figures (17)  Tables (2)
    • Figure 1. 

      Computational details and the coordinate system. (a) Flame structure in side view. (b) Disposition of the pyrolysis zone in top view.

    • Figure 2. 

      Computed and experimental profiles of soot volume fraction for ethylene flame at different locations x along the height z.

    • Figure 3. 

      Profiles of the surface temperature of (a)heptane and (b) dodecane as a function of time at U0 = 0.2 m/s.

    • Figure 4. 

      Spatial distribution of the computed pyrolysis rate over (a) heptane and (b) dodecane surfaces for the different times at U0 = 0.2 m/s.

    • Figure 5. 

      Computed burning rates of (a) heptane and (b) dodecane at the steady mode as a function of oxidizer flow velocity.

    • Figure 6. 

      Impact of oxidizer flow velocity on (a) HRRPUA, (b)combustion efficiency and radiation fraction at the steady mode.

    • Figure 7. 

      Evolution of the convective fraction of HRRPUA over pyrolysis surface for different oxidizer flow velocity.

    • Figure 8. 

      Impact of oxidizer flow velocity on radiant heat flux over material surface at the steady mode.

    • Figure 9. 

      Computed fields of gas temperature above 600 °C for heptane and dodecane at the steady mode (t = 10 s) at U0 = 0.2 m/s.

    • Figure 10. 

      Computed fields of soot volume fraction above 7 ppm on the axis of symmetry at U0 = 0.2 m/s.

    • Figure 11. 

      Computed fields of (a) gas temperature and (b) soot volume fraction (above 2 ppm) on the cross-stream plane for heptane flame at x/Lp = 2 for U0 = 0.2 m/s.

    • Figure 12. 

      Evolution of the mean value of soot volume fraction (ppm) in the windward direction as a function of oxidizer flow velocity.

    • Figure 13. 

      Impact of oxidizer flow velocity on soot deposition (g/m2) over wall surface in the windward direction.

    • Figure 14. 

      Computed fields of CO volume fraction for heptane and dodecane flames at U0 = 0.2 m/s.

    • Figure 15. 

      Influence of oxidizer flow speed on the mean level of CO volume fraction in the forward direction.

    • Figure 16. 

      Unburnt hydrocarbons field calculated at U0 = 0.2 m/s for heptane and dodecane flames.

    • Figure 17. 

      Impact of oxidizer flow velocity on the mean concentration of unburnt hydrocarbons in the forward direction.

    • Fuel typeLSP (m)Af
      Ethylene (C2H4)0.1064.1 × 10−5
      Heptane (C7H16)0.1472.9 × 10−5
      Dodecane (C12H26)0.1373.1 × 10−5

      Table 1. 

      Summary of LSP height and pre-exponential factor, Af, for three types of fuel.

    • PropertyHeptaneDodecane
      Conductivity k (W/m·K)0.170.14
      Density ρ (kg/m3)684750
      Heat capacity Cp (kJ/kg·K)2.242.21
      Pyrolysis heat, Lv (kJ/kg)321256
      Heat of combustion, ΔHc (kJ/kg)4450044147
      Boiling temperature Tb (°C)98216

      Table 2. 

      Thermo-physical and combustion properties of heptane and dodecane.