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Thermophysics and Aeromechanics

2013 year, number 1

Numerical investigation of the flow of ultradisperse particles of the aluminum oxide in the solid-fuel rocket engine nozzle

A.A. Glazunov, N.N. Dyachenko, and L.I. Dyachenko
Tomsk State University, Tomsk, Russia
Dr.Dyachenko@gmail.com
Keywords: distribution function of particles over their sizes, coagulation, fragmentation, two-phase losses
Pages: 81-88

Abstract

The work deals with the two-phase flow investigation. The computations were done for a continuous coagulation model within the framework of the phenomenological multi-fluid model of the medium. A conclusion was drawn that the diminution of the particles size leads to a reduction of two-phase losses in the nozzle unit of the solid-fuel engine.