dc.contributor.author |
Bennett, Christopher J. |
|
dc.contributor.author |
Lawson, Nicholas J. |
|
dc.contributor.author |
Gautrey, James E. |
|
dc.contributor.author |
Cooke, Alastair K. |
|
dc.date.accessioned |
2017-03-20T09:37:54Z |
|
dc.date.available |
2017-03-20T09:37:54Z |
|
dc.date.issued |
2017-03-16 |
|
dc.identifier.citation |
C.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 577-587 |
en_UK |
dc.identifier.issn |
1270-9638 |
|
dc.identifier.uri |
http://dx.doi.org/10.1016/j.ast.2017.03.014 |
|
dc.identifier.uri |
https://dspace.lib.cranfield.ac.uk/handle/1826/11617 |
|
dc.description.abstract |
A 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.language.iso |
en |
en_UK |
dc.publisher |
Elsevier |
en_UK |
dc.rights |
Attribution-NonCommercial-NoDerivatives 4.0 International |
|
dc.rights.uri |
http://creativecommons.org/licenses/by-nc-nd/4.0/ |
|
dc.title |
CFD simulation of flow around angle of attack and sideslip angle vanes on a BAe Jetstream 3102 - Part 2 |
en_UK |
dc.type |
Article |
en_UK |
dc.identifier.cris |
17050220 |
|