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Laminar-Turbulent Transition Modeling Strategies for Thermally Protected Airfoils

[+] Author Affiliations
Luiz Tobaldini Neto

Embraer S.A., São José dos Campos, SP, Brazil

Marcos de Mattos Pimenta, Guilherme Araujo Lima da Silva

Escola Politécnica da Universidade de São Paulo, São Paulo, SP, Brazil

Paper No. FEDSM2008-55284, pp. 451-459; 9 pages
doi:10.1115/FEDSM2008-55284
From:
  • ASME 2008 Fluids Engineering Division Summer Meeting collocated with the Heat Transfer, Energy Sustainability, and 3rd Energy Nanotechnology Conferences
  • Volume 1: Symposia, Parts A and B
  • Jacksonville, Florida, USA, August 10–14, 2008
  • Conference Sponsors: Fluids Engineering Division
  • ISBN: 978-0-7918-4840-1 | eISBN: 0-7918-3832-3
  • Copyright © 2008 by ASME

abstract

The present article discusses some of the transition modeling strategies typically applied by the industry. Transition effects on the heat transfer characteristics and calculation for airfoil anti-ice protection systems build the framework of the developments of interest. Results of the studied models are presented for flat plate data taken from the ERCOFTAC experiments.

Copyright © 2008 by ASME

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