Turbulent separated flow over and downstream of a two-element airfoil

D. Adair, W. C. Horne

Research output: Contribution to journalArticlepeer-review

10 Citations (Scopus)

Abstract

Flow characteristics in the vicinity of the flap of a single-slotted airfoil are presented and analysed. The flow remained attached over the model surfaces except in the vicinity of the flap trailing edge where a small region of boundary-layer separation extended over the aft 7% of flap chord. The airfoil configuration was tested at a Mach number of 0.09 and a chord Reynolds number of 1.8 × 106 in the NASA Ames Research Center 7- by 10-Foot Wind Tunnel. The flow was complicated by the presence of a strong, initially inviscid, jet, emanating from the slot between airfoil and flap, and a gradual merging of the main airfoil wake and flap suction-side boundary layer.

Original languageEnglish
Pages (from-to)531-541
Number of pages11
JournalExperiments in Fluids
Volume7
Issue number8
DOIs
Publication statusPublished - Sep 1 1989
Externally publishedYes

ASJC Scopus subject areas

  • Computational Mechanics
  • Mechanics of Materials
  • Physics and Astronomy(all)
  • Fluid Flow and Transfer Processes

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