Evaluation AC2-08

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Premixed Methane-Air Swirl Burner (TECFLAM)

Application Challenge 2-08 © copyright ERCOFTAC 2011

In order to assess the simulation a comparison of the time averaged velocity, temperature and species distribution with experimental data is presented in this section. A more extensive evaluation can be found in [#Xkuenne_les_2011 Kuenne et�al.]�([#Xkuenne_les_2011 2011]).

Comparison of CFD Results with Experimental Data

In Fig. 5.1 the simulation results of the axial velocity for the isothermal and reacting case are compared with experimental data. As is typical for this type of swirl flow, the velocity field starts to expand right after the nozzle exit, which produces a positive pressure gradient in the axial and radial direction, high enough to form a central recirculation zone as intended for flame stabilization. Overall the spreading of the turbulent swirling flow and the size and intensity of the recirculation zone are well predicted and an excellent agreement with the measurements can be observed in all axial planes for both cases. Comparing the isothermal and reacting case a strong acceleration of the velocity caused by the thermal expansion through the flame front can be observed which is accurately reproduced by the simulation.

Figure 5.1: Comparison of isothermal (left) and reacting (right) flow field. Time averaged axial velocity (u_mean) obtained by the LES ([#Xkuenne_les_2011 Kuenne et�al.]�([#Xkuenne_les_2011 2011])) using the efficiency function of [#Xcharlette_power-law_2002 Charlette et�al.]�([#Xcharlette_power-law_2002 2002]) (solid lines) and [#Xcolin_thickened_2000 Colin et�al.]�([#Xcolin_thickened_2000 2000]) (dashed lines) in comparison with experimental data (dots).

In Fig. 5.2 the temperature and methane mass fraction are compared with experimental data. Since the flame is very sharp the distribution is almost completely caused by the flame-turbulence interaction resulting in a wide turbulent flame brush. Except that a small radial offset exists and the gradient at higher axial positions is slightly over predicted the temperature is well predicted by the simulation. The mean profile of the methane mass fraction reflects its consumption by the chemical reaction on the left and the mixing with the coflowing air on the right. At the higher axial positions the methane mass fraction exceeds the measurement indicating insufficient fuel consumption in the simulation.

Figure 5.2: Temperature (left) and methane mass fraction (right). Time averaged values obtained by the LES ([#Xkuenne_les_2011 Kuenne et�al.]�([#Xkuenne_les_2011 2011])) using the efficiency function of [#Xcharlette_power-law_2002 Charlette et�al.]�([#Xcharlette_power-law_2002 2002]) (solid lines) and [#Xcolin_thickened_2000 Colin et�al.]�([#Xcolin_thickened_2000 2000]) (dashed lines) in comparison with experimental data (dots).

Comparing the efficiency functions (which is the main model parameter) the differences (marked with arrows in Fig.5.1 and 5.2) between the two formulations are small and hence the model uncertainty will not influence the results crucially.

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Contributors: Johannes Janicka (EKT), Guido Kuenne (EKT), Andreas Dreizler (RSM)

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