Helicopter blade twist control through sma technology: optimal shape prediction, twist actuator realisation and main rotor enhanced performance computation

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dc.contributor.authorPagano, A.
dc.contributor.authorAmeduri, S.
dc.contributor.authorCokonaj, V.
dc.contributor.authorPrachar, A.
dc.contributor.authorZachariadis, Z.
dc.contributor.authorDrikakis, D.
dc.date.accessioned2016-06-29T14:39:22Z
dc.date.available2016-06-29T14:39:22Z
dc.date.issued2009
dc.identifier.otherERF;2009-101297
dc.identifier.urihttp://hdl.handle.net/20.500.11881/130
dc.language.isoen
dc.subject.otherActive Rotors
dc.titleHelicopter blade twist control through sma technology: optimal shape prediction, twist actuator realisation and main rotor enhanced performance computation

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