Aksencer, TolgaAydogdu, Metin2024-06-122024-06-1220190263-82231879-1085https://doi.org/10.1016/j.compstruct.2019.111174https://hdl.handle.net/20.500.14551/23674The mechanics of a laminated composite beam attached to inside of a rotating rim and directed to the inward direction is investigated. The Ritz method is utilized in the solution of the problem. Simple algebraic polynomials are used in the displacement field. Clamped-free boundary conditions are considered. First, Reddy (third order) and classical beam theories are used in the formulation. Cross-ply lamination configurations are considered. Effects of rotation speed, hub ratio, orthotropy ratio, beam theory and length to thickness ratio are analyzed in detail. Mode shapes of composite rotating beams are given. It is obtained that composite beams may buckle due to compressive centrifugal force for the some combinations of rotation speed and hub ratio.en10.1016/j.compstruct.2019.111174info:eu-repo/semantics/closedAccessRotating BeamsCompositeVibrationBucklingRitz MethodPly Laminated BeamsCantileverRodsArticle225Q1WOS:0004803304000572-s2.0-85067687550Q1