STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS

The key components in aircraft will be subjected to typical asymmetric loads in service,thus their fatigue behavior can be inevitably strongly affected by the mean stress effect. The modified Walker model employs the multiple-nonlinearfitting method to deal with fatigue test data under various stres...

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Main Authors: SU YunLai, LU Shan, DONG DengKe, CHEN XianMin, CHEN Li
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2021-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2021.02.021
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author SU YunLai
LU Shan
DONG DengKe
CHEN XianMin
CHEN Li
author_facet SU YunLai
LU Shan
DONG DengKe
CHEN XianMin
CHEN Li
author_sort SU YunLai
collection DOAJ
description The key components in aircraft will be subjected to typical asymmetric loads in service,thus their fatigue behavior can be inevitably strongly affected by the mean stress effect. The modified Walker model employs the multiple-nonlinearfitting method to deal with fatigue test data under various stress ratios,by which the influence of material and maximum stress on mean stress effect can both be considered. Eighteen sets of fatigue test data from twelve kinds of aeronautical materials in various loading conditions were employed to validate the predict accuracy of modified Walker model,and the results were compared with other commonly used models. The study shows that the influence of maximum stress on mean stress effect varies with materials,while the prediction accuracy of the modified Walker model for each group of test data is better than that any other candidate models to varying degrees.
format Article
id doaj-art-5921333447d94589aa6ee9d9eb9fd4ac
institution Kabale University
issn 1001-9669
language zho
publishDate 2021-01-01
publisher Editorial Office of Journal of Mechanical Strength
record_format Article
series Jixie qiangdu
spelling doaj-art-5921333447d94589aa6ee9d9eb9fd4ac2025-01-15T02:26:19ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692021-01-014339740330610385STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADSSU YunLaiLU ShanDONG DengKeCHEN XianMinCHEN LiThe key components in aircraft will be subjected to typical asymmetric loads in service,thus their fatigue behavior can be inevitably strongly affected by the mean stress effect. The modified Walker model employs the multiple-nonlinearfitting method to deal with fatigue test data under various stress ratios,by which the influence of material and maximum stress on mean stress effect can both be considered. Eighteen sets of fatigue test data from twelve kinds of aeronautical materials in various loading conditions were employed to validate the predict accuracy of modified Walker model,and the results were compared with other commonly used models. The study shows that the influence of maximum stress on mean stress effect varies with materials,while the prediction accuracy of the modified Walker model for each group of test data is better than that any other candidate models to varying degrees.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2021.02.021Fatigue lifeMean stress effectModified Walker modelMultiple nonlinear fitting
spellingShingle SU YunLai
LU Shan
DONG DengKe
CHEN XianMin
CHEN Li
STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS
Jixie qiangdu
Fatigue life
Mean stress effect
Modified Walker model
Multiple nonlinear fitting
title STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS
title_full STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS
title_fullStr STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS
title_full_unstemmed STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS
title_short STRESS-BASED FATIGUE LIFE MODEL UNDER ASYMMETRICAL LOADS
title_sort stress based fatigue life model under asymmetrical loads
topic Fatigue life
Mean stress effect
Modified Walker model
Multiple nonlinear fitting
url http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2021.02.021
work_keys_str_mv AT suyunlai stressbasedfatiguelifemodelunderasymmetricalloads
AT lushan stressbasedfatiguelifemodelunderasymmetricalloads
AT dongdengke stressbasedfatiguelifemodelunderasymmetricalloads
AT chenxianmin stressbasedfatiguelifemodelunderasymmetricalloads
AT chenli stressbasedfatiguelifemodelunderasymmetricalloads