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Nonisothermal elasto-visco-plastic response of shell-type structuresA mathematical model and solution methodologies for analyzing structural response of thin, metallic shell-type structures under large transient, cyclic or static thermomechanical loads is disussed. Among the system responses, which are associated with these load conditions, are thermal buckling and creep buckling. Thus, geometric as well as material-type nonlinearities (of high order) can be anticipated and have been considered in the development of the mathematical model. Furthermore, this was accommodated in the solution procedures. A complete true ab-inito rate theory of kinematics and kinetics for continuum and curved thin structures, without any restriction on the magnitude of the strains or the deformation, was formulated. The time dependence and large strain behavior are incorporated through the introduction of the time rates of the metric and curvature in two coordinate systems, a fixed (spatial) one and a convected (material) coordinate system. The relations between the time derivative and the covariant derivatives (gradients) have been developed for curved space and motion, so that the velocity components supply the connection between the equations of motion and the time rate of change of the metric and curvature tensors.
Document ID
19870013363
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Simitses, G. J.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Carlson, R. L.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Riff, R.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Lewis Research Center Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Structural Mechanics
Accession Number
87N22796
Funding Number(s)
CONTRACT_GRANT: NAG3-534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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