Heat transfer in the rectangular passage with 60-degree ribs and film holes

Guang Chao Li, Hui Ren Zhu, Tao Guo

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

Numerical simulation was conducted to investigate heat transfer in a rectangular channel with both 60-degree rib-roughened wall and film hole suctions with Reynolds number of 9 × 104 and suction ratio of 0.22. A finite volume method with unstructured meshes was used to solve the three dimensional compressible Navier-Stokes equations. The realizable k-ε model was used carefully and the enhanced wall function was utilized for near wall treatment. The numerical results agree well with the experimental data of the surface with both ribs and film holes. Based on this, investigation was focused on the heat transfer of three other surfaces. The numerical result shows that the flow of the passage is very complex. Heat transfer is enhanced because of the ribs. Maximum Heat transfer coefficient is found on the smooth right surface but not the surfaces with ribs.

Original languageEnglish
Pages (from-to)995-1000
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume21
Issue number6
StatePublished - Dec 2006

Keywords

  • Aerospace propulsion system
  • Aircraft engines
  • Film holes
  • Heat transfer
  • Internal cooling passage
  • Numerical simulation
  • Ribs

Fingerprint

Dive into the research topics of 'Heat transfer in the rectangular passage with 60-degree ribs and film holes'. Together they form a unique fingerprint.

Cite this