CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 2

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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.accessioned2017-03-20T09:37:54Z
dc.date.available2017-03-20T09:37:54Z
dc.date.issued2017-03-16
dc.description.abstractA previous study analysing the local flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 turboprop is extended to study the additional effects of bank angle. A full matrix of CFD simulations is carried out to investigate how the introduction of a bank angle affects vane performance for a range of flight conditions. An updated calibration method to convert the raw vane readings into true values of angle of attack and sideslip, incorporating a correction factor as a function of the bank angle, is presented. The results are shown to be accurate for a wide range of flight configurations. Uncertainty analysis indicates that raw vanes reading errors should be below ±0.1°±0.1° to ensure that total calibration errors are restricted to less than 2%2% for angle of attack and 5%5% for sideslip angle.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 2, Aerospace Science and Technology, Volume 68, September 2017, Pages 577-587en_UK
dc.identifier.cris17050220
dc.identifier.issn1270-9638
dc.identifier.urihttp://dx.doi.org/10.1016/j.ast.2017.03.014
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/11617
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 2en_UK
dc.typeArticleen_UK

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