Flow control on a thick airfoil using suction compared to blowing

Chunmei Chen, Roman Seele, Israel J Wygnanski

Research output: Contribution to journalArticle

19 Citations (Scopus)

Abstract

The effects of steady slot suction as a means of controlling separation on a blunt elliptical airfoil were investigated and compared to the effects of steady blowing applied to the same airfoil previously investigated. Slots whose width approaches 1% of the chord and are located downstream of the natural separation location generate the highest lift for a given dimensionless mass-flow coefficient CQ. This holds true whether the flow separates near the leading edge due to high incidence or near the trailing edge due to the bluntness of the airfoil and is contrary to the observations made when blowing was used. Lift generated by suction through a moderately wide slot located downstream of the natural separation line depends only on CQ, but if the slot is located upstream of the separation line it depends on Reynolds number as well. Contrary to separation control by blowing no deleterious effects were observed at low levels of suction regardless of the suction-slot location. Adding a wedge to the blunt trailing edge of this airfoil enhances the effectiveness of suction, whereas making blowing less effective at low momentum inputs thus increasing the gap between these two approaches to flow separation.

Original languageEnglish (US)
Pages (from-to)1462-1472
Number of pages11
JournalAIAA Journal
Volume51
Issue number6
DOIs
StatePublished - Jun 2013

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Blow molding
Airfoils
Flow control
Flow separation
Momentum
Reynolds number

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Flow control on a thick airfoil using suction compared to blowing. / Chen, Chunmei; Seele, Roman; Wygnanski, Israel J.

In: AIAA Journal, Vol. 51, No. 6, 06.2013, p. 1462-1472.

Research output: Contribution to journalArticle

Chen, Chunmei ; Seele, Roman ; Wygnanski, Israel J. / Flow control on a thick airfoil using suction compared to blowing. In: AIAA Journal. 2013 ; Vol. 51, No. 6. pp. 1462-1472.
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