In this section, the methane-air reaction mechanism from GRI-Mech 3.0 [1] is used. The reaction mechanism consists of 325 reactions that involve 53 species. The three following problems were solved to make comparison of our results with independent calculations.
Parameters of the this problem are similar to that studied in [2]. We don’t concern about the main subject of the work [2] (creating a reduced reaction mechanism for NO emission) and take only the numerical data for NO reburning. A fixed pressure problem is solved.
Pressure: 1 atm
Temperature: 1300K or 1600K
|
CH4 |
C2H6 |
O2 |
NO |
H2O |
N2 |
|
2.864E-03 |
2.98E-04 |
5.09E-03 |
9.47E-04 |
2.16E-02 |
0.9692 |
Comparison of Chemked calculation with data from [2] is given in Fig. 1.
Conditions of this calculation correspond to the experiments [3].
Temperature: 1805K
Gas mixture: [CH2O]0 : [AR]0 = 4 : 96
AR concentration is 1.9E-05 mol/cm3

Fig 2. Normalized CH2O profile:
circles – experimental data [3], line – calculation [1],
crosses – Chemked calculation
Conditions of this calculation correspond to the experiments [4].
Pressure: 1atm
Temperature: 2454K
Gas mixture:
[CH4]0 : [O2]0 : [AR ]0 = 0.1
: 0.4 : 99.5

Fig 3. Mole fraction of CH3:
black line – experiments [4], green line – calculation [1],
crosses – Chemked calculation
[1] GRI-Mech 3.0, The Gas Research Institute,
http://www.me.berkeley.edu/gri_mech/
[2] C.J.Sung, C:K:Law and J.-Y.Chen,, Augmented reduced Mechanism
for NO Emission in Methane Oxidation,
http://mae1.cwru.edu/mae/Pages/Facilities/CDL/ARM-NO_(Final).pdf
[3] Y. Hidaka , T. Taniguchi, H. Tanaka, T. Kamesawa, K. Inami,
and H. Kawano, Combust. Flame 92, 365 (1993).
[4] A.Y. Chang, D.F. Davidson, M. DiRosa, R.K. Hanson, and C.T.
Bowman, "Shock Tube Experiments for Development and Validation of
Kinetic Models of Hydrocarbon Oxidation", (1994) 25th Symposium
(International) on Combustion, Poster 3 - 23.