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Anisotropic constitutive modeling for nickel base single crystal superalloy Rene N4 at 982 C

Authors :
Stouffer, D. C
Jayaraman, N
Sheh, M. Y
Alden, D
Source :
NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987.
Publication Year :
1987
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1987.

Abstract

A back stress/drag stress constitutive model based on a crystallographic approach to model single crystal anisotropy is presented. Experimental results demonstrated the need for the back stress variable in the inelastic flow equations. Experimental findings suggested that back stress is orientation dependent and controls both strain hardening and recovery characteristics. Due to the observed stable fatigue loops at 1800 F, drag stress is considered constant for this temperature. The constitutive model operated with constraints determined only from tensile data was extensively tested from simple tensile and fatigue to complicated strain hold tests. The model predicted very well under those conditions.

Subjects

Subjects :
Metallic Materials

Details

Language :
English
Database :
NASA Technical Reports
Journal :
NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987
Publication Type :
Report
Accession number :
edsnas.19890007953
Document Type :
Report