Modal control of cantilever beam using a gyrostabilizer

MakaleAçık ErişimScopus SJRQ2

Özet

In this paper, an experimental model of a horizontal cantilever beam with a rotating/oscillating attached to the shaker for harmonic excitation at the one end and a gyrostabilizer at the other end is built to verify the equations of the Lagrangian model. The primary focus of the study was to investigate the parameters of excitation amplitude, natural frequency, rotating mass (disk mass), and disk speed of gyro that would minimize the amplitude of the beam to identify these effects. Numerical and experimental results indicate that the angular momentum of the gyrostabilizer is the most effective parameter in the reduction of beam displacement.

Anahtar Kelimeler

RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/12902Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.32604/sv.2021.015705Yayıncı resmi DOI adresi
Atıflar
Scopus
5
WoS
3
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Tam Kayıt
AlanDeğerDil
dc.contributor.authorÇuvalci, Olkan
dc.contributor.authorÜnker, Faruk
dc.contributor.authorBaturalp, Turgut Batuhan
dc.contributor.authorGülbulak, Utku
dc.contributor.authorErtas, Atila
dc.date.accessioned2026-10-22T10:20:41.293479127Z
dc.date.available2026-10-22T10:20:41.293479127Z
dc.date.issued2021
dc.description.abstractIn this paper, an experimental model of a horizontal cantilever beam with a rotating/oscillating attached to the shaker for harmonic excitation at the one end and a gyrostabilizer at the other end is built to verify the equations of the Lagrangian model. The primary focus of the study was to investigate the parameters of excitation amplitude, natural frequency, rotating mass (disk mass), and disk speed of gyro that would minimize the amplitude of the beam to identify these effects. Numerical and experimental results indicate that the angular momentum of the gyrostabilizer is the most effective parameter in the reduction of beam displacement.
dc.identifier.doi10.32604/sv.2021.015705
dc.identifier.endpage294
dc.identifier.issn1541-0161
dc.identifier.issue4
dc.identifier.scopus2-s2.0-85118312812
dc.identifier.startpage281
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/12902
dc.identifier.volume55
dc.identifier.wosWOS:000708857500002
dc.language.isoen
dc.publisherTech Science Press
dc.relation.ispartofSound and Vibration
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectCantilever beam
dc.subjectFlexural vibration
dc.subjectGyrostabilizer
dc.subjectModal control
dc.subjectRoll motion
dc.subjectRotating tip mass
dc.subject.classificationAcoustics
dc.subject.classificationEngineering, Mechanical
dc.subject.classificationMechanics
dc.subject.classificationEngineering
dc.subject.otherLagrange multipliers
dc.subject.otherNanocantilevers
dc.subject.otherExcitation amplitudes
dc.subject.otherExperimental modelling
dc.subject.otherFlexural vibrations
dc.subject.otherHarmonic excitation
dc.subject.otherLagrangian models
dc.subject.otherModal control
dc.subject.otherRoll motions
dc.subject.otherRotating mass
dc.subject.otherRotating tip mass
dc.subject.otherTip mass
dc.subject.otherCantilever beams
dc.titleModal control of cantilever beam using a gyrostabilizer
dc.typeArticle
dspace.entity.typePublication
rdl.citation.scopus5
rdl.citation.wos3
rdl.oa.statusgold
rdl.oa.urlhttps://doi.org/10.32604/sv.2021.015705
rdl.scopus.quartileQ2
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexEmerging Sources Citation Index (ESCI)