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

Garry, Kevin; Di Pasquale, Davide; Prince, Simon A.; Lawson, Nicholas J.

CERES Home
→
School of Aerospace, Transport and Manufacturing (SATM)
→
Staff publications (SATM)
→
View Item

dc.contributor.author	Garry, Kevin
dc.contributor.author	Di Pasquale, Davide
dc.contributor.author	Prince, Simon A.
dc.contributor.author	Lawson, Nicholas J.
dc.date.accessioned	2019-03-13T14:42:25Z
dc.date.available	2019-03-13T14:42:25Z
dc.date.issued	2018-12-31
dc.identifier.citation	Garry 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, Brazil	en_UK
dc.identifier.isbn	978-3-932182-88-4
dc.identifier.uri	https://dspace.lib.cranfield.ac.uk/handle/1826/13985
dc.identifier.uri	https://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0297.htm
dc.description	© The Author.
dc.description.abstract	SPIV 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.language.iso	en	en_UK
dc.publisher	ICAS	en_UK
dc.rights	Attribution 4.0 International
dc.rights	© The Author.
dc.rights.uri	http://creativecommons.org/licenses/by/4.0/
dc.subject	High-Lift	en_UK
dc.subject	Wake vortex	en_UK
dc.subject	SPIV	en_UK
dc.title	The influence of high-speed SPIV data processing parameters on aircraft wing vortex wake assessment	en_UK
dc.type	Conference paper	en_UK