The results of the first year of work on a program to validate unified constitutive models for isotropic materials utilized in high temperature regions of gas turbine engines and to demonstrate their usefulness in computing stress-strain-time-temperature histories in complex three-dimensional structural components. The unified theories combine all inelastic strain-rate components in a single term avoiding, for example, treating plasticity and creep as separate response phenomena. An extensive review of existing unified theories is given and numerical methods for integrating these stiff time-temperature-dependent constitutive equations are discussed. Two particular models, those developed by Bodner and Partom and by Walker, were selected for...
Development of a simplified method for estimating structural inelastic stress and strain response to...
The purpose is to develop life prediction models for coated anisotropic materials used in gas temper...
Complex states of stress and strain are introduced into components during service in engineering app...
The third and fourth years of a 4-year research program, part of the NASA HOST Program, are describe...
The results of the third year of work on a program which is part of the NASA Hot Section Technology ...
Unified constitutive material models were developed for structural analyses of aircraft gas turbine ...
Unified constitutive models are characterized by the use of a single inelastic strain rate term for ...
Thermomechanical service conditions for high-temperature levels, thermal transients, and mechanical ...
An uncoupled constitutive model for predicting the transient response of thermal and rate dependent,...
Four current viscoplastic models are compared experimentally with Inconel 718 at 1100 F. A series of...
Single crystal materials are being used in gas turbine airfoils and are candidates for other hot sec...
Notched members were tested at temperatures far above those recorded till now. Simulation of the not...
The purpose of this program is to develop life prediction models for coated anisotropic materials us...
Current gas turbine engines utilize large single crystal superalloy components in the hot section. S...
Effects of inelastic materials models on computed stress-strain solutions for thermally loaded struc...
Development of a simplified method for estimating structural inelastic stress and strain response to...
The purpose is to develop life prediction models for coated anisotropic materials used in gas temper...
Complex states of stress and strain are introduced into components during service in engineering app...
The third and fourth years of a 4-year research program, part of the NASA HOST Program, are describe...
The results of the third year of work on a program which is part of the NASA Hot Section Technology ...
Unified constitutive material models were developed for structural analyses of aircraft gas turbine ...
Unified constitutive models are characterized by the use of a single inelastic strain rate term for ...
Thermomechanical service conditions for high-temperature levels, thermal transients, and mechanical ...
An uncoupled constitutive model for predicting the transient response of thermal and rate dependent,...
Four current viscoplastic models are compared experimentally with Inconel 718 at 1100 F. A series of...
Single crystal materials are being used in gas turbine airfoils and are candidates for other hot sec...
Notched members were tested at temperatures far above those recorded till now. Simulation of the not...
The purpose of this program is to develop life prediction models for coated anisotropic materials us...
Current gas turbine engines utilize large single crystal superalloy components in the hot section. S...
Effects of inelastic materials models on computed stress-strain solutions for thermally loaded struc...
Development of a simplified method for estimating structural inelastic stress and strain response to...
The purpose is to develop life prediction models for coated anisotropic materials used in gas temper...
Complex states of stress and strain are introduced into components during service in engineering app...