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Stability and dynamical analysis of whirl flutter in a gimballed rotor-nacelle system with a smooth nonlinearity – CORRIGENDUM

Published online by Cambridge University Press:  29 August 2023

C. Mair ,
D. Rezgui  and
B. Titurus
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Abstract

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Keywords

Whirl flutterBifurcationsContinuationTiltrotorAeroelasticity
Type
Corrigendum
Information
The Aeronautical Journal , First View , pp. 1
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Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (https://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution and reproduction, provided the original article is properly cited.
Copyright
© The Author(s), 2023. Published by Cambridge University Press on behalf of Royal Aeronautical Society

The originally published article was missing complete grant information. The initial acknowledgements read as follows:

‘Acknowledgements. The authors would like to kindly thank The UK Engineering and Physical Sciences Research Council (EPSRC) for funding this research project. Further thanks are extended to Dr David Barton and Prof. Alan Champneys for lending their expertise on torus bifurcations and quasi-periodic behaviour, crucial to this work.’

This should be:

‘Acknowledgements. The authors would like to kindly thank The UK Engineering and Physical Sciences Research Council (EPSRC) for funding this research project, under grant number: EP/N509619/1. Further thanks are extended to Dr David Barton and Prof. Alan Champneys for lending their expertise on torus bifurcations and quasi-periodic behaviour, crucial to this work.’

References

Mair, C., Rezgui, D. and Titurus, B. (2023). Stability and dynamical analysis of whirl flutter in a gimballed rotor-nacelle system with a smooth nonlinearity. The Aeronautical Journal, 127, 1234–1254. https://doi.org/10.1017/aer.2023.10 CrossRefGoogle Scholar