A time-splitting method for the numerical simulation of stiff nonequilibrium combustion problem was developed. The algorithm has been applied to simulate the shock-induced combustion and to investigate a supersonic one- and two-phase flowfield. The results are physically reasonable and demonstrate that the presence of particles has a dramatic effect on the nozzle flowfield and the the thrust. Copyright (C) 1997 Elsevier Science Ltd.
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER