Lift curve breakdown for airfoil undergoing dynamic stall

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dc.contributor.authorChoudhry, A.
dc.contributor.authorArjomandi, M.
dc.contributor.authorKelso, R.
dc.contributor.conference19th Australasian Fluid Mechanics Conference (AFMC) (8 Dec 2014 - 11 Dec 2014 : Melbourne, Vic.)
dc.date.issued2014
dc.description.abstractThe work presented aims to investigate the lift-characteristics of a thick airfoil section undergoing dynamic stall. The NACA 0021 airfoil was selected for the experimental work performed at the KC Wind Tunnel at the University of Adelaide. The airfoil was pitched at the mid-chord and the unsteady surface pressure distributions were recorded. The surface pressures were then used to obtain the lift-curve for the airfoil undergoing dynamic stall. In the present article, the unsteady lift-curve has been broken down into stages and each stage has been analysed to gain a deeper understanding of the dynamic stall lift.
dc.description.statementofresponsibilityA. Choudhry, M. Arjomandi, and R. Kelso
dc.identifier.citationProceedings of the 19th Australasian Fluid Mechanics Conference, 2014, pp.1-4
dc.identifier.isbn9780646596952
dc.identifier.orcidArjomandi, M. [0000-0002-7669-2221]
dc.identifier.orcidKelso, R. [0000-0002-5783-9232]
dc.identifier.urihttp://hdl.handle.net/2440/92006
dc.language.isoen
dc.publisherAustralasian Fluid Mechanics Society
dc.rightsCopyright status unknown
dc.source.urihttp://people.eng.unimelb.edu.au/imarusic/proceedings/19/100.pdf
dc.titleLift curve breakdown for airfoil undergoing dynamic stall
dc.typeConference paper
pubs.publication-statusPublished

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