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Effects of a kind of non-smooth blade on the performance of an axial fan

  • Hongwei Ma*
  • , Jibo Guo
  • *Corresponding author for this work
  • National Key Laboratory on Aero-Engines
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

This paper presents an experimental investigation of effects of a kind of streamwise-grooved blade on the performance of an axial-flow fan. The flow field at 25% chord downstream from the trailing edge at hub was measured using a 5-hole pressure probe at different mass-flow conditions. The fan performance of the groove blades was compared with that of the smooth blades. The measurement results indicate that: (1) the non-smooth blades increase mass flow of the fan at the same throttle conditions except a near stall condition; (2) the non-smooth blades reduce the relative total pressure loss in the rotor passage and increase the fan's total pressure rise at the test mass-flow conditions except the near stall condition; (3) Negative benefits are obtained at a near stall condition when the smooth blades are replaced by the non-smooth ones. The fan mass flow decreases 0.9% while the total-pressure rise decreases 2.4% at the near stall condition.

Original languageEnglish
Pages (from-to)200-205
Number of pages6
JournalJournal of Thermal Science
Volume15
Issue number3
DOIs
StatePublished - Sep 2006

Keywords

  • Aerodynamic performance
  • Axial fan
  • Non-smooth blade
  • Streamwise groove

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