Discharge coefficient of 3-in-1 hole with various inclination angle and hole pitch

Guangchao Li, Huiren Zhu, Huiming Fan

Research output: Contribution to journalArticlepeer-review

6 Scopus citations

Abstract

Discharge coefficients of 3-in-1 hole of three inclination angles and three spacing between holes are presented which described the discharge behavior of a row of holes. The inlet and outlet of the 3-in-1 hole both have a 15° lateral expansion. The flow conditions considered are mainstream turbulence intensities and density ratios of secondary flow to mainstream. The momentum flux ratios varied in the range from 1 to 4. The comparison is made of the discharge coefficients of three shaped holes to find an optimal hole with low flow loss. The results show that the discharge coefficients of 3-in-1 hole are highest in three shaped holes and therefore this article is focused on the measurements of discharge coefficients of 3-in-1 hole for various geometries and aerodynamic parameters. The measured results of 3-in-1 hole indicate that turbulence intensities, density ratios and momentum flux ratios have weak influence on discharge coefficients for inclination angle of 20°. The high turbulence intensity yields the small discharge coefficients for inclination angle of 45° and 90°. The increased both momentum flux ratios and density ratios lead to the increased discharge coefficients for inclination angle of 45° and 90°. The increased inclination angle causes the rapidly increased discharge coefficients. There is a weak dependence of discharge coefficients on hole pitches.

Original languageEnglish
Pages (from-to)385-392
Number of pages8
JournalChinese Journal of Aeronautics
Volume21
Issue number5
DOIs
StatePublished - Oct 2008

Keywords

  • Aerospace propulsion system
  • Discharge coefficient
  • Film cooling hole
  • Gas turbine

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