New model to calculate the film cooling effectiveness

Hui Ren Zhu, Song Ling Liu

Research output: Contribution to journalArticlepeer-review

Abstract

A new mixing model for the discrete-hole injection process description was suggested with the conception of equivalent boundary layer and parameters of jet out ratio. This injection model was incorporated in a two-dimensional boundary layer code using the low Reynolds number k-ε two-equation turbulent model. The computation was carried out smoothly with the use of equivalent boundary layer. The conception of jet out ratio was used to account for the effect of cooling air penetrated through boundary layer. The calculation results show that the new model could be used to compute the film cooling effectiveness of discrete-hole injection process with higher blowing ratios.

Original languageEnglish
Pages (from-to)51-54
Number of pages4
JournalTuijin Jishu/Journal of Propulsion Technology
Volume24
Issue number1
StatePublished - Feb 2003

Keywords

  • Cooled blade
  • Equivalent boundary layer
  • Film cooling
  • Jet mixing flow
  • Jet out ratio
  • Mixing model

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