Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel

Multiaxial asynchronous fatigue experiments were carried out on 30CrMnSiA steel to investigate the influence of frequency ratio on fatigue crack initiation and propagation. Test results show that the surface cracks initiate on the maximum shear stress amplitude planes with larger normal stress, prop...

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Main Authors: Tianqi Liu, Xinxin Qi, Xinhong Shi, Limin Gao, Tian Zhang, Jianyu Zhang
Format: Article
Language:English
Published: MDPI AG 2021-07-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/14/14/3968
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spelling doaj-6ee33a0159214645bedd99d500e675352021-07-23T13:51:52ZengMDPI AGMaterials1996-19442021-07-01143968396810.3390/ma14143968Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA SteelTianqi Liu0Xinxin Qi1Xinhong Shi2Limin Gao3Tian Zhang4Jianyu Zhang5School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing 100191, ChinaBeijing Key Laboratory of Civil Aircraft Structures and Composite Materials, COMAC Beijing Aircraft Technology Research Institute, Beijing 102211, ChinaBeijing Key Laboratory of Civil Aircraft Structures and Composite Materials, COMAC Beijing Aircraft Technology Research Institute, Beijing 102211, ChinaCollege of Aerospace Engineering, Chongqing University, Chongqing 400044, ChinaMultiaxial asynchronous fatigue experiments were carried out on 30CrMnSiA steel to investigate the influence of frequency ratio on fatigue crack initiation and propagation. Test results show that the surface cracks initiate on the maximum shear stress amplitude planes with larger normal stress, propagate approximately tens of microns, and then propagate along the maximum normal stress planes. The frequency ratio has an obvious effect on the fatigue life. The variation of normal and shear stress amplitudes on the maximum normal stress plane induces the crack retardation, and results in that the crack growth length is longer for the constant amplitude loading than that for the asynchronous loading under the same fatigue life ratio. A few fatigue life prediction models were employed and compared. Results show that the fatigue life predicted by the model of Bannantine-Socie cycle counting method, section critical plane criterion and Palmgren-Miner’s cumulative damage rule were more applicable.https://www.mdpi.com/1996-1944/14/14/396830CrMnSiA steelcrack growth pathfatigue life predictionasynchronous loadingfrequency ratio
collection DOAJ
language English
format Article
sources DOAJ
author Tianqi Liu
Xinxin Qi
Xinhong Shi
Limin Gao
Tian Zhang
Jianyu Zhang
spellingShingle Tianqi Liu
Xinxin Qi
Xinhong Shi
Limin Gao
Tian Zhang
Jianyu Zhang
Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel
Materials
30CrMnSiA steel
crack growth path
fatigue life prediction
asynchronous loading
frequency ratio
author_facet Tianqi Liu
Xinxin Qi
Xinhong Shi
Limin Gao
Tian Zhang
Jianyu Zhang
author_sort Tianqi Liu
title Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel
title_short Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel
title_full Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel
title_fullStr Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel
title_full_unstemmed Effect of Loading Frequency Ratio on Multiaxial Asynchronous Fatigue Failure of 30CrMnSiA Steel
title_sort effect of loading frequency ratio on multiaxial asynchronous fatigue failure of 30crmnsia steel
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2021-07-01
description Multiaxial asynchronous fatigue experiments were carried out on 30CrMnSiA steel to investigate the influence of frequency ratio on fatigue crack initiation and propagation. Test results show that the surface cracks initiate on the maximum shear stress amplitude planes with larger normal stress, propagate approximately tens of microns, and then propagate along the maximum normal stress planes. The frequency ratio has an obvious effect on the fatigue life. The variation of normal and shear stress amplitudes on the maximum normal stress plane induces the crack retardation, and results in that the crack growth length is longer for the constant amplitude loading than that for the asynchronous loading under the same fatigue life ratio. A few fatigue life prediction models were employed and compared. Results show that the fatigue life predicted by the model of Bannantine-Socie cycle counting method, section critical plane criterion and Palmgren-Miner’s cumulative damage rule were more applicable.
topic 30CrMnSiA steel
crack growth path
fatigue life prediction
asynchronous loading
frequency ratio
url https://www.mdpi.com/1996-1944/14/14/3968
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