An experimental study of a plunging airfoil in the post stall region

dc.contributor.authorRasi, Marzabadi F.
dc.contributor.authorSoltani, M.R.
dc.date.accessioned2014-12-10T06:33:35Z
dc.date.available2014-12-10T06:33:35Z
dc.date.issued2007
dc.description.abstractPaper presented at the 5th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, South Africa, 1-4 July, 2007.en_ZA
dc.description.abstractA series of low speed wind tunnel tests were conducted to study the unsteady flow events on an airfoil oscillating in plunge mode beyond its static-stall angle of attack. Data were acquired at a Reynolds number of 0.42*106, over a range of reduced frequencies, k=0.03-0.1 and plunging amplitude of ±15cm. It was found that in the post stall region, there existed a fully separated flow over the upper surface of the airfoil and the dynamic stall vortex formed in the vicinity of the leading edge region. Also, the effect of the reduced frequency was investigated.
dc.description.librariancs2014en_ZA
dc.format.extent6 pagesen_ZA
dc.format.mediumPDFen_ZA
dc.identifier.citationRasi, MF & Soltani, MR 2007, Experimental study of a plunging airfoil in the post stall region, Paper presented to the 5th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics, South Africa, 1-4 July 2007.en_ZA
dc.identifier.isbn9781868546435
dc.identifier.urihttp://hdl.handle.net/2263/42898
dc.language.isoenen_ZA
dc.publisherInternational Conference on Heat Transfer, Fluid Mechanics and Thermodynamicsen_ZA
dc.relation.ispartofHEFAT 2007
dc.rightsUniversity of Pretoriaen_ZA
dc.rights.uriUniversity of Pretoriaen_US
dc.subjectAirfoil oscillating in plunge modeen_ZA
dc.titleAn experimental study of a plunging airfoil in the post stall regionen_ZA
dc.typePresentationen_ZA

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