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Evaporation of Fuel Droplets in Turbulent Combustor Flow FREE

[+] Author Affiliations
S. Wittig, W. Klausmann, B. Noll, J. Himmelsbach

Universität Karlsruhe (T.H.), Karlsruhe, West-Germany

Paper No. 88-GT-107, pp. V003T06A012; 6 pages
doi:10.1115/88-GT-107
From:
  • ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Amsterdam, The Netherlands, June 6–9, 1988
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7920-7
  • Copyright © 1988 by ASME

abstract

Detailed measurements of a recirculating, droplet charged air flow within a model combustor are compared with predictions based on three different evaporation models. Similar results are obtained with the simplified d2-law, the uniform temperature model and thin skin model for relatively short droplet-heatup phases. Discrepancies, however, are observed under conditions where the droplet heating phase is relatively long, i.e. at low temperature conditions. Extended evaporation models, therefore, are necessary when the ignition performance is to be analysed.

Copyright © 1988 by ASME
This article is only available in the PDF format.

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