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Free vibration analysis of a rotating Timoshenko beam by differential transform method

dc.contributor.authorKaya, Metin O.
dc.contributor.ituauthorKaya, Metin Orhan
dc.date.accessioned2026-01-25T23:43:34Z
dc.date.issued2006-05-01
dc.description.abstractPurposeTo perform the flapwise bending vibration analysis of a rotating cantilever Timoshenko beam.Design/methodology/approachKinetic and potential energy expressions are derived step by step. Hamiltonian approach is used to obtain the governing equations of motion. Differential transform method (DTM) is applied to solve these equations.FindingsIt is observed that the ρIΩ2θ term which is ignored by many researchers and which becomes more important as the rotational speed parameter increases must be included in the formulation.Originality/valueKinetic and potential energy expressions for rotating Timoshenko beams are derived clearly step by step. It is the first time, for the best of author's knowledge, that DTM has been applied to the blade type rotating Timoshenko beams.
dc.description.urihttps://doi.org/10.1108/17488840610663657
dc.description.urihttps://dx.doi.org/10.1108/17488840610663657
dc.identifier.doi10.1108/17488840610663657
dc.identifier.endpage203
dc.identifier.issn0002-2667
dc.identifier.openairedoi_dedup___::a49534cfd0439f8323766ddb97b2bc63
dc.identifier.orcid0000-0003-1589-8100
dc.identifier.startpage194
dc.identifier.urihttps://hdl.handle.net/11527/53038
dc.identifier.volume78
dc.language.isoeng
dc.publisherEmerald
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.rightsCLOSED
dc.titleFree vibration analysis of a rotating Timoshenko beam by differential transform method
dc.typeArticle
dspace.entity.typePublication
person.identifier.orcid0000-0003-1589-8100

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