Difference between revisions of "Multi-inlet kerosene/air flame with scheme"
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Revision as of 18:07, 24 March 2017
Objectives
The Stochastic_ReducedLuche test case shows the reduction of a reduced version of the Luche scheme [1], for a 0D 2-inlet configuration. Started with 43 species and 302 reactions, we reduce to 23 species and 221 reactions.
Principle
The configuration has 2 inlets, one of air and the second one of pure n-decane. The Luche scheme represents the fuel with a composition mainly based on n-decane (~77%) and we choose to start from a 100% n-decane fuel here, in order to run a relatively quick test case. The target species here are , and .
Key parameters
The main parameters are found in the condition.cpp file.
configuration = "MultipleInlet"; step = "DRGEP_species";
When you perform the next steps, the given mech is the one chosen from the previously step.
mech= "mechanisms/luche_red_43s.xml"; mech_desc = "luche";
//Inlet 1
listInlets.push_back(new MultipleInlet(
/*Temperature*/ 750,
/*Pressure*/ 1E+05,
/*Mass flow rate*/ 0.500,
/*Xk*/ "O2:0.2321, N2:0.7679",
/*Yk*/ "",
/**/ false,
/**/ 0.0,
/**/ 0.0,
/**/ 0.0,
/**/ 0.0));
//Inlet 2
listInlets.push_back(new MultipleInlet(
/*Temperature*/ 750,
/*Pressure*/ 1E+05,
/*Mass flow rate*/ 0.017,
/*Xk*/ "NC10H22:1.0",
/*Yk*/ "",
/**/ true,
/**/ 1.28E-05,
/**/ 4.91E-4,
/**/ 810,
/**/ 251000));
A third inlet is set for the burned gases, with the composition calculated at equilibrium.
//BurnedGases
listInlets.push_back(new Characteristics_MultipleInlet(
/*Temperature*/ 2000,
/*Pressure*/ 1E+05,
/*Mass flow rate*/ 0.200,
/*Xk*/ "N2:0.76308, O2:0.093573, H2O:0.072355, CO2:0.070468",
/*Yk*/ "",
/**/ false,
/**/ 0.0,
/**/ 0.0,
/**/ 0.0,
/**/ 0.0,
/*tau_t*/ 2e-04,
/*delta_t*/ 1e-05,
/*nbIterations*/ 200,
/*BurnedGases*/ true));
Be careful, the new_mixing parameter must be set to true only for the first step (DRGEP_species in that case).
new_mixing = true;
Results
DRGEP step
The DRGEP_Species step ranks the species as follows
Bibliography
- ↑ J. Luche. Elaboration of reduced kinetic models of combustion. Application to a kerosene mechanism. PhD thesis, LCSR Orleans, 2003.