Bennett, Christopher J.Lawson, Nicholas J.Gautrey, James E.Cooke, Alastair K.2017-03-202017-03-202017-03-16C.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 577-5871270-9638http://dx.doi.org/10.1016/j.ast.2017.03.014https://dspace.lib.cranfield.ac.uk/handle/1826/11617A 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.enAttribution-NonCommercial-NoDerivatives 4.0 Internationalhttp://creativecommons.org/licenses/by-nc-nd/4.0/Article17050220