Several theories of creep and creep rupture are reviewed. Specific attention is devoted to the brittle damage theory proposed by Kachanov. Creep, damage and life predictions for rectangular or circular cross section beams under bending and tensile loads are presented. Comparison with data for a Ni Superalloy showed life predictions could be 30X in excess of experimental values. This beam model also revealed that it is imperative that no bending moments be inadvertently applied during tensile creep testing. The creep-damage material model is extended to multidimensional situations. A refinement, whereby no damage accumulates in compression, is incorporated. A User-Material subroutine for this constitutive model has been formulated, and incor...
To capture the mechanical response of Ni-based materials, creep deformation and rupture experiments ...
Inspection and maintenance of industrial gas turbines (IGTs) cost millions of dollars. Growing deman...
The method presented in WADD TR 60-411 Part I for predicting deformations in aircraft structures und...
Bibliography: pages 92-98.In this thesis a simplified analysis procedure is developed, in which cree...
The deformation of structural alloys presents problems for power plants and aerospace applications d...
The creep of materials is a research topic of major significance in the life assessment and design o...
ABSTRACT: In this work an original creep prediction model is presented with a unified comprehensive...
AbstractThe assessment of crack initiation and propagation under creep conditions is important in th...
The deformation of structural alloys presents problems for power plants and aerospace applications d...
International audienceThe prediction of the creep behaviour and life of components of aeronautic eng...
Creep rupture strength values are basis for design in many high temperature applications. The applic...
Inspection and maintenance of industrial gas turbines (IGTs) cost millions of dollars. Growing deman...
AbstractThe paper critically examines the advantages and limitations of empirical and constitutive e...
To capture the mechanical response of Ni-based materials, creep deformation and rupture experiments ...
The deformation of structural alloys presents problems for power plants and aerospace applications d...
To capture the mechanical response of Ni-based materials, creep deformation and rupture experiments ...
Inspection and maintenance of industrial gas turbines (IGTs) cost millions of dollars. Growing deman...
The method presented in WADD TR 60-411 Part I for predicting deformations in aircraft structures und...
Bibliography: pages 92-98.In this thesis a simplified analysis procedure is developed, in which cree...
The deformation of structural alloys presents problems for power plants and aerospace applications d...
The creep of materials is a research topic of major significance in the life assessment and design o...
ABSTRACT: In this work an original creep prediction model is presented with a unified comprehensive...
AbstractThe assessment of crack initiation and propagation under creep conditions is important in th...
The deformation of structural alloys presents problems for power plants and aerospace applications d...
International audienceThe prediction of the creep behaviour and life of components of aeronautic eng...
Creep rupture strength values are basis for design in many high temperature applications. The applic...
Inspection and maintenance of industrial gas turbines (IGTs) cost millions of dollars. Growing deman...
AbstractThe paper critically examines the advantages and limitations of empirical and constitutive e...
To capture the mechanical response of Ni-based materials, creep deformation and rupture experiments ...
The deformation of structural alloys presents problems for power plants and aerospace applications d...
To capture the mechanical response of Ni-based materials, creep deformation and rupture experiments ...
Inspection and maintenance of industrial gas turbines (IGTs) cost millions of dollars. Growing deman...
The method presented in WADD TR 60-411 Part I for predicting deformations in aircraft structures und...