Attempts to use complex chemistry and transport in direct numerical simulat
ions (DNS) of premixed combustion (even for kinetically simple systems, suc
h as H-2/air and CH4/air) often result in excessive needs of memory and CPU
time. This paper presents a methodology (integrated combustion chemistry [
ICC]) capable of integrating complex chemistry effects into DNS while maint
aining computational efficiency. The methodology includes the use of a limi
ted number of species and reactions with parameters which are derived to ma
tch a number of flame properties. It is illustrated through a four-step rea
ction mechanism appropriate for a stoichiometric methane/air flame, and whi
ch compares favorably with predictions of the detailed GRI 2.11 mechanism.
The proposed scheme includes one reaction for the methane oxidation, one fo
r the thermal, one for the Fenimore, and one for the nonpremixed reburn che
mical NOx routes. The kinetic parameters for the hydrocarbon oxidation were
determined by matching the GRI 2.11 predictions for laminar burning veloci
ty and adiabatic flame temperature, main reactants concentrations, and exti
nction strain rates for both premixed (steady) and nonpremixed (steady and
unsteady) strained laminar flames. The chemical parameters for the three st
eps corresponding to NOx chemistry were determined by matching the NOx prof
iles obtained for strained diffusion flames with GRI 2.11. Finally, this fo
ur-step mechanism was used in DNS of two- and three-dimensional turbulent n
onpremixed combustion to assess the validity of flamelet approaches. While
the flamelet approaches were found to perform well for heat release, their
extension to NOx formation appears to be not as successful because of the e
xistence of compressed zones where products accumulate and increase the NOx
production. (C) 1999 by The Combustion Institute.