This paper, which is the first of two in a series, provides an overview of a viscoplastic constitutive model that accounts for time-dependent material deformation (e.g., creep, stress relaxation, etc.) in monolithic ceramics. Using continuum principles of engineering mechanics the complete theory is derived from a scalar dissipative potential function first proposed by Robinson (1978), and later utilized by Duffy (1988). Derivations based on a flow potential function provide an assurance that the inelastic boundary value problem is well posed, and solutions obtained are unique. The specific formulation used here for the threshold function (a component of the flow potential function) was originally proposed by Willam and Warnke (1975) in order to formulate constitutive equations for time-independent classical plasticity behavior observed in cement and unreinforced concrete. Here constitutive equations formulated for the flow law (strain rate) and evolutionary law employ stress invariants to define the functional dependence on the Cauchy stress and a tensorial state variable. This particular formulation of the viscoplastic model exhibits a sensitivity to hydrostatic stress, and allows different behavior in tension and compression.
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ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
June 10–13, 1996
Birmingham, UK
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7873-6
PROCEEDINGS PAPER
A Viscoplastic Constitutive Theory for Monolithic Ceramics: I Free
Lesley A. Janosik,
Lesley A. Janosik
NASA Lewis Research Center, Cleveland, OH
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Stephen F. Duffy
Stephen F. Duffy
Cleveland State University, Cleveland, OH
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Lesley A. Janosik
NASA Lewis Research Center, Cleveland, OH
Stephen F. Duffy
Cleveland State University, Cleveland, OH
Paper No:
96-GT-368, V002T04A007; 11 pages
Published Online:
February 6, 2015
Citation
Janosik, LA, & Duffy, SF. "A Viscoplastic Constitutive Theory for Monolithic Ceramics: I." Proceedings of the ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. Birmingham, UK. June 10–13, 1996. V002T04A007. ASME. https://doi.org/10.1115/96-GT-368
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