The aircraft spin - a mathematical approach and comparison to flight test
| dc.contributor.author | Bennett, Christopher J. | |
| dc.contributor.author | Lawson, Nicholas J. | |
| dc.contributor.author | Gautrey, Jim | |
| dc.contributor.author | Cooke, Alastair | |
| dc.date.accessioned | 2017-06-27T10:59:15Z | |
| dc.date.available | 2017-06-27T10:59:15Z | |
| dc.date.issued | 2017-06-09 | |
| dc.description.abstract | A Scottish Aviation Bulldog light aircraft operated by the National Flying Laboratory Centre (NFLC) at Cran eld University, modi ed with research equipment including bre optic sensors for wing strain and fuselage pressure measurements, is used to investigate the dynamics of a fully developed spin. A theoretical model is developed to compare with existing ight test data. In particular, the frequency of the aircraft spin is analysed as a function of the mass distribution of the aircraft to determine the e ect of the fuel load. It is found that the spin frequency is minimally a ected by the fuel load since the moments of inertia corresponding to the engine, for example, are far more signi cant. However, it is con rmed that the yawing e ect of the propeller causes the aircraft to spin faster to the right than to the left. | en_UK |
| dc.identifier.citation | Christopher J. Bennett, Nicholas Lawson, Jim Gautrey and Alastair Cooke. The aircraft spin - a mathematical approach and comparison to flight test. AIAA Flight Testing Conference: AIAA AVIATION Forum 2017, 5-9 June 2017, Denver, Colorado, USA. | en_UK |
| dc.identifier.issn | http://dx.doi.org/10.2514/6.2017-3652 | |
| dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/12113 | |
| dc.language.iso | en | en_UK |
| dc.publisher | American Institute of Aeronautics and Astronautics | en_UK |
| dc.rights | Attribution-Non-Commercial 3.0 Unported (CC BY-NC 3.0) You are free to: Share — copy and redistribute the material in any medium or format, Adapt — remix, transform, and build upon the material. The licensor cannot revoke these freedoms as long as you follow the license terms. Under the following terms: Attribution — You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use. Information: Non-Commercial — You may not use the material for commercial purposes. No additional restrictions — You may not apply legal terms or technological measures that legally restrict others from doing anything the license permits. | |
| dc.title | The aircraft spin - a mathematical approach and comparison to flight test | en_UK |
| dc.type | Conference paper | en_UK |