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A Modeling Investigation of Thermal and Strain Induced Recovery and Nonlinear Hardening in Potential Based ViscoplasticitySpecific forms for both the Gibb's and the complementary dissipation potentials were chosen such that a complete potential based multiaxial, isothermal, viscoplastic model was obtained. This model in general possesses three internal state variables (two scalars associated with dislocation density and one tensor associated with dislocation motion) both thermal and dynamic recovery mechanisms, and nonlinear kinematic hardening. This general model, although possessing associated flow and evolutionary laws, is shown to emulate three distinct classes of theories found in the literature, by modification of the driving threshold function F. A parametric study was performed on a specialized nondimensional multiaxial form containing only a single tensorial internal state variable (i.e., internal stress). The study was conducted with the idea of examining the impact of including a strain-induced recovery mechanism and the compliance operator, derived from the Gibb's potential, on the uniaxial and multiaxial response. One important finding was that inclusion of strain recovery provided the needed flexibility in modeling stress-strain and creep response of metals at low homologous temperatures, without adversely affecting the high temperature response. Furthermore, for nonproportional loading paths, the inclusion of the compliance operator had a significant influence on the multiaxial response, but had no influence on either uniaxial or proportional load histories.
Document ID
19940007010
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Arnold, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Saleeb, A. F.
(Akron Univ. OH., United States)
Wilt, T. E.
(Toledo Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
E-7786
NAS 1.15:106122
NASA-TM-106122
Report Number: E-7786
Report Number: NAS 1.15:106122
Report Number: NASA-TM-106122
Accession Number
94N11482
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Public Use Permitted.
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