Modeling Viscoelastic Behavior Using Flexible Multibody Dynamics Formulations

dc.contributor.advisorBauchau, Olivier Prof.en_US
dc.contributor.authorNemani, Nishanten_US
dc.contributor.departmentAerospace Engineeringen_US
dc.contributor.publisherDigital Repository at the University of Marylanden_US
dc.contributor.publisherUniversity of Maryland (College Park, Md.)en_US
dc.date.accessioned2021-09-16T05:30:21Z
dc.date.available2021-09-16T05:30:21Z
dc.date.issued2020en_US
dc.description.abstractViscoelastic behavior is frequently observed in dynamical flexible multibody systems. In the simplest form it is manifested in one dimensional revolute and prismatic joints. Beyond which more complex force elements such as six degree of freedom flexible joints can also be found. Finally, beams, plates and shells are found to exhibit viscoelastic behavior too. In the past extensive work has been done on analyzing the dynamic response of three dimensional beams by performing cross-sectional analysis through finite element methods and subsequently solving the reduced beam problem. The approach is particularly relevant for the analysis of complex cross sections and helps improve computational efficiency significantly. A formulation which incorporates a viscoelastic model of the generalized Maxwell type with a solution of the three dimensional beam theory which gives an exact solution of static three dimensional elasticity problems is presented. Multiple examples incorporating the use of the aforementioned model in the context of viscoelastic beams and joints are presented. Shortcomings of the Kelvin-Voigt model, which is often used for flexible multibody systems, are underlined.en_US
dc.identifierhttps://doi.org/10.13016/o6jh-z3jg
dc.identifier.urihttp://hdl.handle.net/1903/27696
dc.language.isoenen_US
dc.subject.pqcontrolledEngineeringen_US
dc.subject.pqcontrolledAerospace engineeringen_US
dc.subject.pquncontrolledDynamicsen_US
dc.subject.pquncontrolledViscoelasticityen_US
dc.titleModeling Viscoelastic Behavior Using Flexible Multibody Dynamics Formulationsen_US
dc.typeThesisen_US

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