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Towards a Numerical Study of Two-Phase Flow Exhaust Plume Jet

[+] Author Affiliations
C. Devals, J.-L. Estivalezes

ONERA/DMAE/MH, Toulouse Cedex, France

G. Jourdan, L. Houas

Université de Provence, Marseille Cedex, France

Paper No. FEDSM2002-31028, pp. 491-496; 6 pages
doi:10.1115/FEDSM2002-31028
From:
  • ASME 2002 Joint U.S.-European Fluids Engineering Division Conference
  • Volume 1: Fora, Parts A and B
  • Montreal, Quebec, Canada, July 14–18, 2002
  • Conference Sponsors: Fluids Engineering Division
  • ISBN: 0-7918-3615-0 | eISBN: 0-7918-3600-2
  • Copyright © 2002 by ASME

abstract

The aim of the present work is to determine experimental drag coefficients for spherical particles accelerated in shock-tube. Then, validations of two phase flow calculations dealing with solid propulsion rocket in supersonic flight are undertaken. First, experiments in the multi-phase vertical-horizontal shock-tube have been set up at IUSTI in Marseille. The drag coefficient is determinated for particle Reynolds numbers less than 50000 and for particle Mach numbers less than 1.14 and is compared with those found in literature. Second, calculation of two phase flow in solid rocket plume has been performed. The particles are tracked with a stochastic one-way coupling lagrangian method.

Copyright © 2002 by ASME

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