An approach is presented to combine a system of criteria and combustion mod
els into a computer tool for conservative estimates of possible pressure lo
ads resulting from combustion of fuel-air mixtures. This approach is based
on identification of characteristic combustion regimes by their relative se
verity, application of criteria to identify the strongest possible regime f
or particular initial conditions and geometry, and on development of approp
riate three-dimensional models to describe flame propagation and loads for
selected combustion regimes. A computer code (CREBCOM) was developed using
this approach. Short descriptions of the code, criteria and models are give
n. The computer code was applied to simulate turbulent deflagration and det
onation experiments at different scale and geometrical configurations. Thes
e experiments included tests with flame propagation in explosion channels (
tubes) and large-scale tests in the RUT facility. Numerical simulations sho
wed that such a code is able to give reliable estimations of overpressure f
or a wide range of combustion regimes, compositions and geometry. (C) 2001
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