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A viscoelastic higher-order beam finite elementA viscoelastic internal variable constitutive theory is applied to a higher-order elastic beam theory and finite element formulation. The behavior of the viscous material in the beam is approximately modeled as a Maxwell solid. The finite element formulation requires additional sets of nodal variables for each relaxation time constant needed by the Maxwell solid. Recent developments in modeling viscoelastic material behavior with strain variables that are conjugate to the elastic strain measures are combined with advances in modeling through-the-thickness stresses and strains in thick beams. The result is a viscous thick-beam finite element that possesses superior characteristics for transient analysis since its nodal viscous forces are not linearly dependent an the nodal velocities, which is the case when damping matrices are used. Instead, the nodal viscous forces are directly dependent on the material's relaxation spectrum and the history of the nodal variables through a differential form of the constitutive law for a Maxwell solid. The thick beam quasistatic analysis is explored herein as a first step towards developing more complex viscoelastic models for thick plates and shells, and for dynamic analyses. The internal variable constitutive theory is derived directly from the Boltzmann superposition theorem. The mechanical strains and the conjugate internal strains are shown to be related through a system of first-order, ordinary differential equations. The total time-dependent stress is the superposition of its elastic and viscous components. Equations of motion for the solid are derived from the virtual work principle using the total time-dependent stress. Numerical examples for the problems of relaxation, creep, and cyclic creep are carried out for a beam made from an orthotropic Maxwell solid.
Document ID
19960028587
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Johnson, Arthur R.
(Army Research Lab. Hampton, VA United States)
Tressler, Alexander
(NASA Langley Research Center Hampton,VA United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-110260
NAS 1.15:110260
ARL-MR-325
Report Number: NASA-TM-110260
Report Number: NAS 1.15:110260
Report Number: ARL-MR-325
Meeting Information
Meeting: MAFELAP Conference
Location: Uxbridge
Country: United Kingdom
Start Date: June 25, 1996
End Date: June 28, 1996
Accession Number
96N29312
Funding Number(s)
PROJECT: RTOP 505-63-53-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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