Modeling crack initiation and propagation in nickel base superalloys

Nickel base superalloys are the primary class of materials used in the manufacture of high temperature components for gas turbine aeroengines, including combustion casings and liners, guide vane and turbine blades and dics, etc. These components are subjected to complex cyclic loading induced by the...

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Váldodahkkit: Korsunsky, A, Song, X, Belnoue, J, Prakash, L, Dini, D, Walsh, M
Materiálatiipa: Conference item
Almmustuhtton: Trans Tech Publications Inc. 2007
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author Korsunsky, A
Song, X
Belnoue, J
Prakash, L
Dini, D
Walsh, M
author_facet Korsunsky, A
Song, X
Belnoue, J
Prakash, L
Dini, D
Walsh, M
author_sort Korsunsky, A
collection OXFORD
description Nickel base superalloys are the primary class of materials used in the manufacture of high temperature components for gas turbine aeroengines, including combustion casings and liners, guide vane and turbine blades and dics, etc. These components are subjected to complex cyclic loading induced by the combination of mechanical loading, changing temperatures and thermal gradients, inducing plastic deformation and creep, that ultimately may lead to crack initiation and propagation. The purpose of the present paper is to provide a necessarily brief overview of recent modeling activities in this field, including polycrystalline crystal plasticity modeling for the study of crack initiation, coupled non-local damage-plasticity modeling for crack initiation and propagation studies, and the incorporation of time and environment dependent processes (creep and oxidation) in the predictive modeling of fatigue crack growth rates in nickel base superalloys).
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spelling oxford-uuid:6e4d7672-23f4-4fcc-b51b-835b6d24cc2c2022-03-26T19:23:34ZModeling crack initiation and propagation in nickel base superalloysConference itemhttp://purl.org/coar/resource_type/c_5794uuid:6e4d7672-23f4-4fcc-b51b-835b6d24cc2cSymplectic Elements at OxfordTrans Tech Publications Inc.2007Korsunsky, ASong, XBelnoue, JPrakash, LDini, DWalsh, MNickel base superalloys are the primary class of materials used in the manufacture of high temperature components for gas turbine aeroengines, including combustion casings and liners, guide vane and turbine blades and dics, etc. These components are subjected to complex cyclic loading induced by the combination of mechanical loading, changing temperatures and thermal gradients, inducing plastic deformation and creep, that ultimately may lead to crack initiation and propagation. The purpose of the present paper is to provide a necessarily brief overview of recent modeling activities in this field, including polycrystalline crystal plasticity modeling for the study of crack initiation, coupled non-local damage-plasticity modeling for crack initiation and propagation studies, and the incorporation of time and environment dependent processes (creep and oxidation) in the predictive modeling of fatigue crack growth rates in nickel base superalloys).
spellingShingle Korsunsky, A
Song, X
Belnoue, J
Prakash, L
Dini, D
Walsh, M
Modeling crack initiation and propagation in nickel base superalloys
title Modeling crack initiation and propagation in nickel base superalloys
title_full Modeling crack initiation and propagation in nickel base superalloys
title_fullStr Modeling crack initiation and propagation in nickel base superalloys
title_full_unstemmed Modeling crack initiation and propagation in nickel base superalloys
title_short Modeling crack initiation and propagation in nickel base superalloys
title_sort modeling crack initiation and propagation in nickel base superalloys
work_keys_str_mv AT korsunskya modelingcrackinitiationandpropagationinnickelbasesuperalloys
AT songx modelingcrackinitiationandpropagationinnickelbasesuperalloys
AT belnouej modelingcrackinitiationandpropagationinnickelbasesuperalloys
AT prakashl modelingcrackinitiationandpropagationinnickelbasesuperalloys
AT dinid modelingcrackinitiationandpropagationinnickelbasesuperalloys
AT walshm modelingcrackinitiationandpropagationinnickelbasesuperalloys