Vibration reduction of a Lynx aircraft via actively controlled trailing edge flaps
Vibration reduction of a Lynx aircraft via actively controlled trailing edge flaps
Jones, Mark P.
36095656-977b-4cd0-a738-3f9e36fe475c
Newman, Simon J.
802c97ed-ea28-477f-8b1e-8e4f873c4281
Jones, Mark P.
36095656-977b-4cd0-a738-3f9e36fe475c
Newman, Simon J.
802c97ed-ea28-477f-8b1e-8e4f873c4281
Jones, Mark P. and Newman, Simon J.
(2006)
Vibration reduction of a Lynx aircraft via actively controlled trailing edge flaps.
32nd European Rotorcraft Forum, ERF 2006, Maastricht, the Netherlands.
11 - 13 Sep 2006.
(Submitted)
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Conference or Workshop Item
(Paper)
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Submitted date: September 2006
Venue - Dates:
32nd European Rotorcraft Forum, ERF 2006, Maastricht, the Netherlands, 2006-09-11 - 2006-09-13
Identifiers
Local EPrints ID: 26816
URI: http://eprints.soton.ac.uk/id/eprint/26816
PURE UUID: 786f772c-8d07-4eb4-a7c4-5f69410503b1
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Date deposited: 06 Feb 2007
Last modified: 11 Dec 2021 15:02
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Contributors
Author:
Mark P. Jones
Author:
Simon J. Newman
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