Reference : Limit Cycle Oscillation Control

	Document type :	Scientific congresses and symposiums : Poster
	Discipline(s) :	Engineering, computing & technology : Aerospace & aeronautics engineering Engineering, computing & technology : Mechanical engineering
	To cite this reference:	http://hdl.handle.net/2268/25510

Title :	Limit Cycle Oscillation Control
Language :	English
Author, co-author :	Dimitriadis, Grigorios [Université de Liège - ULg > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
Publication date :	Dec-2000
Page number :	A0
On invitation :	No
Audience :	National
Event name :	Poster Presentation and Reception for Britain's Younger Engineers
Event date :	6 December 2000
Event organizer :	House of Commons
Event place (city) :	London
Event country :	United Kingdom
Keywords :	[en] Limit Cycle Oscillations ; Control Systems ; Suppression
Abstract :	[en] Over the last fifteen years the Aerospace industry has started to show a continuously increasing interest in the investigation of the vibrations of aircraft subjected to nonlinear structural and aerodynamic forces. Here, a control scheme designed to alleviate or even stop some types of nonlinear aircraft vibrations is presented.
Target :	Researchers ; Professionals
Permalink :	http://hdl.handle.net/2268/25510

	File(s) associated to this reference
	Fulltext file(s): File Commentary Version Size Access Restricted access 05 BYE 2000.pdf Author preprint 174.59 kB Request copy

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