Now showing items 1-2 of 2

    • Boundary-layers integral analysis - Heated airfoils in icing conditions  (Trabalho apresentado em evento)

      Da Silva, Guilherme Araújo Lima; De Mattos Silvares, Otávio; De Jesus Zerbini, Euryale Jorge Godoy (American Institute of Aeronautics and Astronautics Inc., 2008)
      Under icing conditions, it is necessary to heat and control the temperature of the airfoil surface at leading edge region to prevent ice formation. The thermal anti-ice system balances mainly the evaporative cooling effects, ...
    • Heat transfer on iced cylinders  (Trabalho apresentado em evento)

      Stefanini, Luciano Martinez; Silvares, Otávio de Mattos; da Silva, Guilherme Araujo Lima; de jesus Zerbini, Euryale Jorge Godoy (AIAA International, 2010)
      The convective heat transfer is the main mechanism to remove the solidification enthalpy during glaze ice accretion. Most of the airfoil icing prediction codes use a heat transfer calculation procedure based on the classical ...