Dynamic wind turbine model including blade oscillation effects for control strategy enabling mechanical stress reduction

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dc.contributor.author Pournaras, C en
dc.contributor.author Riziotis, V en
dc.contributor.author Kladas, A en
dc.date.accessioned 2014-03-01T02:52:39Z
dc.date.available 2014-03-01T02:52:39Z
dc.date.issued 2010 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/35976
dc.subject.other Aerodynamic models en
dc.subject.other Beam elements en
dc.subject.other Blade elements en
dc.subject.other Blade oscillations en
dc.subject.other Computation time en
dc.subject.other Control strategies en
dc.subject.other Dynamic winds en
dc.subject.other Energy capture en
dc.subject.other In-control en
dc.subject.other Mechanical stress en
dc.subject.other Rotor blades en
dc.subject.other System hardware en
dc.subject.other Turbine models en
dc.subject.other Aeroelasticity en
dc.subject.other Dynamic analysis en
dc.subject.other Dynamics en
dc.subject.other Energy conversion en
dc.subject.other Stresses en
dc.subject.other Turbines en
dc.subject.other Turbomachine blades en
dc.subject.other Wind power en
dc.subject.other Aerodynamics en
dc.title Dynamic wind turbine model including blade oscillation effects for control strategy enabling mechanical stress reduction en
heal.type conferenceItem en
heal.identifier.primary 10.1049/cp.2010.0891 en
heal.identifier.secondary http://dx.doi.org/10.1049/cp.2010.0891 en
heal.publicationDate 2010 en
heal.abstract The paper presents a coupled electrical aerodynamic model for a three blade wind-turbine dynamic analysis. The model is based on a blade element representation of the aerodynamic load part combined with an aeroelastic beam element for the dynamic analysis of a real rotor blade, including top tower acceleration. The model involves reduced computation time enabling to be applied in control system hardware. Such an analysis is very promising for obtaining controllers involving compromises among contradictory targets such as energy capture maximization and mechanical stresses reduction in the aerodynamic part. en
heal.journalName IET Conference Publications en
dc.identifier.doi 10.1049/cp.2010.0891 en
dc.identifier.volume 2010 en
dc.identifier.issue 572 CP en

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