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Vibration reduction of a Lynx aircraft via actively controlled trailing edge flaps

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)

Record type: Conference or Workshop Item (Paper)

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More information

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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