The influence of high-speed SPIV data processing parameters on aircraft wing vortex wake assessment

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dc.contributor.authorGarry, Kevin
dc.contributor.authorDi Pasquale, Davide
dc.contributor.authorPrince, Simon A.
dc.contributor.authorLawson, Nicholas J.
dc.date.accessioned2019-03-13T14:42:25Z
dc.date.available2019-03-13T14:42:25Z
dc.date.issued2018-12-31
dc.description© The Author.
dc.description.abstractSPIV is a powerful tool to assess aircraft wing vortex wakes. Current optical systems enable velocity vector measurements at sample rates of 10Hz. This facilitates detailed assessment of flows containing multiple, potentially unsteady, vortices. SPIV data from the wake of a high-lift wing is used to investigate data sampling strategies on the magnitude of vortex trajectory and strength.en_UK
dc.identifier.citationGarry K, Di Pasquale D, Prince S, Lawson N. (2018) The influence of high-speed SPIV data processing parameters on aircraft wing vortex wake assessment. 31st Congress of the International Council of the Aeronautical Sciences, 9-14 September 2018, Belo Horizonte, Brazilen_UK
dc.identifier.isbn978-3-932182-88-4
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/13985
dc.identifier.urihttps://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0297.htm
dc.language.isoenen_UK
dc.publisherICASen_UK
dc.rightsAttribution 4.0 International
dc.rights© The Author.
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectHigh-Liften_UK
dc.subjectWake vortexen_UK
dc.subjectSPIVen_UK
dc.titleThe influence of high-speed SPIV data processing parameters on aircraft wing vortex wake assessmenten_UK
dc.typeConference paperen_UK

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