Modal control of cantilever beam using a gyrostabilizer
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 adresAtıflar
- Scopus
- 5
- WoS
- 3
Tam Kayıt
| Alan | Değer | Dil |
|---|---|---|
| dc.contributor.author | Çuvalci, Olkan | |
| dc.contributor.author | Ünker, Faruk | |
| dc.contributor.author | Baturalp, Turgut Batuhan | |
| dc.contributor.author | Gülbulak, Utku | |
| dc.contributor.author | Ertas, Atila | |
| dc.date.accessioned | 2026-10-22T10:20:41.293479127Z | |
| dc.date.available | 2026-10-22T10:20:41.293479127Z | |
| dc.date.issued | 2021 | |
| dc.description.abstract | 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. | |
| dc.identifier.doi | 10.32604/sv.2021.015705 | |
| dc.identifier.endpage | 294 | |
| dc.identifier.issn | 1541-0161 | |
| dc.identifier.issue | 4 | |
| dc.identifier.scopus | 2-s2.0-85118312812 | |
| dc.identifier.startpage | 281 | |
| dc.identifier.uri | https://rdlopen.rawdatalibrary.net/r/gumushane/12902 | |
| dc.identifier.volume | 55 | |
| dc.identifier.wos | WOS:000708857500002 | |
| dc.language.iso | en | |
| dc.publisher | Tech Science Press | |
| dc.relation.ispartof | Sound and Vibration | |
| dc.rights | info:eu-repo/semantics/openAccess | |
| dc.subject | Cantilever beam | |
| dc.subject | Flexural vibration | |
| dc.subject | Gyrostabilizer | |
| dc.subject | Modal control | |
| dc.subject | Roll motion | |
| dc.subject | Rotating tip mass | |
| dc.subject.classification | Acoustics | |
| dc.subject.classification | Engineering, Mechanical | |
| dc.subject.classification | Mechanics | |
| dc.subject.classification | Engineering | |
| dc.subject.other | Lagrange multipliers | |
| dc.subject.other | Nanocantilevers | |
| dc.subject.other | Excitation amplitudes | |
| dc.subject.other | Experimental modelling | |
| dc.subject.other | Flexural vibrations | |
| dc.subject.other | Harmonic excitation | |
| dc.subject.other | Lagrangian models | |
| dc.subject.other | Modal control | |
| dc.subject.other | Roll motions | |
| dc.subject.other | Rotating mass | |
| dc.subject.other | Rotating tip mass | |
| dc.subject.other | Tip mass | |
| dc.subject.other | Cantilever beams | |
| dc.title | Modal control of cantilever beam using a gyrostabilizer | |
| dc.type | Article | |
| rdl.citation.scopus | 5 | |
| rdl.citation.wos | 3 | |
| rdl.oa.status | gold | |
| rdl.oa.url | https://doi.org/10.32604/sv.2021.015705 | |
| rdl.scopus.quartile | Q4 | |
| rdl.source.index | SCOPUS | |
| rdl.source.index | WOS | |
| rdl.wos.index | Emerging Sources Citation Index (ESCI) |
