• Title of article

    Effect of Multi-hole Configuration on Film Cooling Effectiveness

  • Author/Authors

    Taheri, Y. Semnan University, Semnan, Iran , Rajabi Zargarabadi, M. Semnan University, Semnan, Iran , Jahromi, M. University Complex of Aerospace Engineering - Malek Ashtar University of Technology, Tehran, Iran

  • Pages
    10
  • From page
    33
  • To page
    42
  • Abstract
    A numerical study is performed to investigate the effects of shaped multi-hole on film cooling effectiveness over a flat plate. Hence a single cylindrical film cooling hole with 11.1 mm diameter is replaced with the shaped multi-hole (14 holes with 2.97 mm diameter) while maintaining constant blowing ratio. Numerical simulations are performed at a fixed density ratio of 1.6, length-to-diameter of 4 and an inclined angle of 35o. Two configurations of hook and fan shapes are considered for multihole. The control-volume method with a semi-implicit method for pressure linked equations-consistent algorithm has been used to solve the steady-state Reynolds-averaged Navier–Stokes equations. The k-ε model is applied for modeling the turbulent flow and heat transfer field. It is found that replacing a single hole with the shaped multi-hole leads to a considerable increase in the film cooling effectiveness in both axial and lateral directions. Results of the present study show that for blowing ratio of 0.6, the hook shape and fan shape configurations of multi-hole, provide a higher area-averaged film cooling effectiveness by 48% and 58.2% more than the single hole respectively.
  • Farsi abstract
    فاقد چكيده فارسي
  • Keywords
    Film cooling , Multi-hole , Adiabatic effectiveness , Numerical simulation
  • Journal title
    AUT Journal of Mechanical Engineering
  • Serial Year
    2019
  • Record number

    2506891