The equations of the Shell model are reexamined with a view to their more e
ffective implementation into a computational fluid dynamics code. The simpl
ification of the solution procedure without compromising accuracy is achiev
ed by replacing time as an independent variable with the fuel depletion, wh
ich is the difference between the initial fuel concentration and the curren
t one. All the other variables used in this model, including temperature, c
oncentration of oxygen, radicals, intermediate and branching agents are exp
ressed as functions of fuel depletion. Equations for the temperature and co
ncentration of the intermediate agent are of the first order and allow anal
ytical solutions. The concentrations of oxygen and fuel are related via an
algebraic equation which is solved in a straightforward way. In this case t
he numerical solution of five coupled first-order ordinary differential equ
ations is reduced to the solution of only two coupled first-order different
ial equations for the concentration of radicals and branching agent. It is
possible to rearrange these equations even further so that the equation for
the concentration of the radicals is uncoupled from the equation for the b
ranching agent. In this case the equation for the concentration of radicals
becomes a second-order ordinary differential equation. This equation is so
lved analytically in two limiting cases and numerically in the general case
. The solution of the first-order ordinary differential equation for the co
ncentration of the branching agent and the solution of the first-order diff
erential equation for time are presented in the form of integrals containin
g the concentration of the radicals obtained earlier. This approach allows
the central processing unit (CPU) time to be more than halved and makes the
calculation of the autoignition process using the Shell model considerably
more effective. (C) 1999 by The Combustion Institute.