Dynamics of hinged wings in strong upward gusts

Jonathan Stevenson, Jorn A. Cheney, James R. Usherwood, Richard J. Bomphrey, Shane P Windsor*

*Corresponding author for this work

Research output: Contribution to journalArticle (Academic Journal)peer-review

1 Citation (Scopus)
133 Downloads (Pure)

Abstract

A bird's wings are articulated to its body via highly mobile shoulder joints. The joints confer an impressive range of motion, enabling the wings to make broad, sweeping movements that can modulate quite dramatically the production of aerodynamic load. This is enormously useful in challenging flight environments, especially the gusty, turbulent layers of the lower atmosphere. In this study, we develop a dynamics model to examine how a bird-scale gliding aircraft can use wing-root hinges (analogous to avian shoulder joints) to reject the initial impact of a strong upward gust. The idea requires that the spanwise centre of pressure and the centre of percussion of the hinged wing start, and stay, in good initial alignment (the centre of percussion here is related to the idea of a ‘sweet spot’ on a bat, as in cricket or baseball). We propose a method for achieving this rejection passively, for which the essential ingredients are (i) appropriate lift and mass distributions; (ii) hinges under constant initial torque; and (iii) a wing whose sections stall softly. When configured correctly, the gusted wings will first pivot on their hinges without disturbing the fuselage of the aircraft, affording time for other corrective actions to engage. We expect this system to enhance the control of aircraft that fly in gusty conditions.
Original languageEnglish
Article number221607
Number of pages16
JournalRoyal Society Open Science
Volume10
Issue number5
DOIs
Publication statusPublished - 10 May 2023

Bibliographical note

Funding Information:
This work received funding from the European Research Council (ERC) under the European Union's Horizon 2020 research and innovation programme (grant agreement no. 679355) and from the Air Force Office of Scientific Research, Air Force Materiel Command, USAF (award no. FA9550-16-1-0034). J.R.U. also received funding from the Wellcome Trust (Fellowship no. 202854/Z/16/Z). Acknowledgements

Publisher Copyright:
© 2023 The Authors.

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