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Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams

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dc.contributor.authorCihan, Melahat
dc.contributor.authorSeher Eken
dc.contributor.authorMetin O. Kaya
dc.contributor.orcid0000-0002-8426-9378
dc.contributor.orcid0000-0002-1868-0791
dc.contributor.orcid0000-0003-1589-8100
dc.date.accessioned2025-11-13T10:52:05Z
dc.date.issued2017-08-18
dc.identifier.doihttps://doi.org/10.1007/s00707-017-1944-y
dc.identifier.endpage4367
dc.identifier.issn0001-5970
dc.identifier.issue12
dc.identifier.openalexW2747733069
dc.identifier.startpage4353
dc.identifier.urihttps://hdl.handle.net/11421/5500
dc.identifier.urihttps://doi.org/10.1007/s00707-017-1944-y
dc.identifier.volume228
dc.language.isoen
dc.relation.ispartofActa Mechanica
dc.rightsrestrictedAccess
dc.subjectFlutter
dc.subjectBending stiffness
dc.subjectSpinning
dc.subjectMaterials science
dc.subjectBeam (structure)
dc.subjectGalerkin method
dc.subjectStructural engineering
dc.subjectSolid mechanics
dc.subjectInstability
dc.subjectStiffness
dc.subjectBending
dc.subjectTransverse plane
dc.subjectMechanics
dc.subjectAerodynamics
dc.subjectPhysics
dc.subjectEngineering
dc.subjectComposite material
dc.subjectFinite element method
dc.subject.sdg7
dc.titleDynamic instability of spinning launch vehicles modeled as thin-walled composite beams
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5083272193

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