CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 1

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dc.contributor.authorBennett, Christopher J.
dc.contributor.authorLawson, Nicholas J.
dc.contributor.authorGautrey, James E.
dc.contributor.authorCooke, Alastair K.
dc.date.accessioned2017-03-20T09:15:02Z
dc.date.available2017-03-20T09:15:02Z
dc.date.issued2017-03-16
dc.description.abstractCFD modelling techniques are exploited to investigate the local velocity field around angle of attack and sideslip angle sensors fitted to the nose of a modified BAe Jetstream 3102 small airliner. Analysis of the flow angularity at the vane locations has allowed the vanes response to varying flight conditions to be predicted and errors in the readings to be quantified. Subsequently, a more accurate calibration of the system is applied to the current configuration on the Jetstream, and a better understanding of the position error with respect to the vane locations is obtained. The above aircraft was acquired by Cranfield University in 2003 with subsequent flow angle vane modifications taking place in 2005. The aircraft is currently in operation with the National Flying Laboratory Centre (NFLC) for research and demonstration purposes.en_UK
dc.identifier.citationC.J. Bennett, N.J. Lawson, J.E. Gautrey, A. Cooke, CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 1, Aerospace Science and Technology, Volume 68, September 2017, Pages 561-576en_UK
dc.identifier.cris17049963
dc.identifier.issn1270-9638
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/11616
dc.identifier.urihttp://dx.doi.org/10.1016/j.ast.2017.03.015
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.titleCFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 1en_UK
dc.typeArticleen_UK

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