Dynamics and stability issues of a synch-rotor aircraft

dc.contributor.author	Avanzini, G.
dc.contributor.author	Bertolani, G.
dc.contributor.author	De Angelis, E.L.
dc.contributor.author	Giulietti, F.
dc.contributor.author	Rossetti, G.
dc.date.accessioned	2024-12-12T18:47:34Z
dc.date.available	2024-12-12T18:47:34Z
dc.date.issued	2021
dc.description.abstract	This paper presents an analytical framework for addressing the stability analysis of a synch-rotor configuration. By linearization about some different trim conditions, a linearized model is obtained made by the decoupled longitudinal and lateral/directional dynamics. A detailed analysis of the stability derivatives and natural modes is given, showing how relevant design parameters, proper of the intermeshing rotors configuration, affect the rotorcraft dynamical behavior. A numerical test case is discussed in support of the proposed model.
dc.identifier.other	ERF-2021-070
dc.identifier.uri	https://hdl.handle.net/20.500.11881/4258
dc.language.iso	en
dc.title	Dynamics and stability issues of a synch-rotor aircraft

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