Abstract
A numerical analysis of supersonic nozzle flows of gas–particle mixtures is described. A time-dependent technique is applied to solve a two-phase inviscid flow through an axially symmetric nozzle. The two-step MacCormack algorithm is used for the gas-phase flow and the method of characteristics is applied to the particle-phase flow. Attention is mainly focused on the location of the limiting particle streamline. The numerical results are compared with the theoretical results obtained previously and also with experiments.
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