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Revisiting the effects of blade geometry on rotor behaviour in descending flight

Revisiting the effects of blade geometry on rotor behaviour in descending flight
Revisiting the effects of blade geometry on rotor behaviour in descending flight
A set of simple, testable hypotheses for the behaviour of the rotor flow in axial flight is derived from a fusion of experimental, numerical and theoretical ideas. Although it is unlikely that all of the results described in this paper will stand up in the face of new information as it becomes available, the series of conundrums, paradoxes (and, simply, questions to be answered) that has been generated by this approach has proved invaluable in focusing research and helping to guide our progress in understanding the complexities of the rotor's aerodynamics - particularly within the vortex ring state.
Newman, S.
802c97ed-ea28-477f-8b1e-8e4f873c4281
Brown, R.
b9108870-6092-4963-b323-be7254c71976
Perry, J.
b5ab7490-06ab-45e9-9a9f-ce51948a9685
Khelifa, M.
d6dade5a-82e0-4f93-8c45-c4f8d686b760
Modha, A.
8519bb2a-d9d9-4314-9953-f769a138c9e7
Arlin, G.
19311dc5-899e-4976-9863-604d160f8fda
Newman, S.
802c97ed-ea28-477f-8b1e-8e4f873c4281
Brown, R.
b9108870-6092-4963-b323-be7254c71976
Perry, J.
b5ab7490-06ab-45e9-9a9f-ce51948a9685
Khelifa, M.
d6dade5a-82e0-4f93-8c45-c4f8d686b760
Modha, A.
8519bb2a-d9d9-4314-9953-f769a138c9e7
Arlin, G.
19311dc5-899e-4976-9863-604d160f8fda

Newman, S., Brown, R., Perry, J., Khelifa, M., Modha, A. and Arlin, G. (2004) Revisiting the effects of blade geometry on rotor behaviour in descending flight. 30th European Rotorcraft Forum, Marseilles. 31 Aug 2004.

Record type: Conference or Workshop Item (Paper)

Abstract

A set of simple, testable hypotheses for the behaviour of the rotor flow in axial flight is derived from a fusion of experimental, numerical and theoretical ideas. Although it is unlikely that all of the results described in this paper will stand up in the face of new information as it becomes available, the series of conundrums, paradoxes (and, simply, questions to be answered) that has been generated by this approach has proved invaluable in focusing research and helping to guide our progress in understanding the complexities of the rotor's aerodynamics - particularly within the vortex ring state.

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More information

Published date: 2004
Venue - Dates: 30th European Rotorcraft Forum, Marseilles, 2004-08-31 - 2004-08-31

Identifiers

Local EPrints ID: 22890
URI: http://eprints.soton.ac.uk/id/eprint/22890
PURE UUID: e83e516a-4d50-4336-8b67-564e3afce543

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Date deposited: 31 Mar 2006
Last modified: 11 Dec 2021 14:41

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Contributors

Author: S. Newman
Author: R. Brown
Author: J. Perry
Author: M. Khelifa
Author: A. Modha
Author: G. Arlin

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