This paper presents the results of a computational investigation of th
e process of deflagration to detonation transition in a combustible ga
s mixture. The type of combustion (i.e., deflagration or detonation) s
upported by a two-step reaction scheme is studied as a function of the
activation energies. It is shown that both a deflagration to detonati
on transition and a deflagration wave that lags behind a leading shock
are possible. Two types of deflagration to detonation transitions are
found theoretically: initiation of detonation from the flame zone and
initiation of detonation along a contact discontinuity in the compres
sed gas near the primary shock wave.