Development of a fatigue crack growth testing apparatus and its application to thin titanium foil
ABSTRACT A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular...
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Published in | Fatigue & fracture of engineering materials & structures Vol. 36; no. 11; pp. 1187 - 1198 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
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Oxford
Blackwell Publishing Ltd
01.11.2013
Blackwell Wiley Subscription Services, Inc |
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Abstract | ABSTRACT
A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular specimens. To illustrate the testing apparatus, mode I fatigue crack growth in 30‐µm‐thick high‐purity titanium foils was studied. Experiments were performed at ambient temperature using a loading frequency of 2 Hz and a nominal stress ratio of 0.1. The cyclic crack growth data could be fit to a Paris relationship between crack growth rate and stress intensity range. The stress intensity factor exponent, m, in the Paris relationship was between 4 and 6, which is comparable with the relatively high values found in the literature for the tension–tension fatigue of other metallic bulk materials. Incomplete self‐similarity analysis was used to explain the observed higher m values for thin metallic foils. |
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AbstractList | A low-cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular specimens. To illustrate the testing apparatus, mode I fatigue crack growth in 30-µm-thick high-purity titanium foils was studied. Experiments were performed at ambient temperature using a loading frequency of 2Hz and a nominal stress ratio of 0.1. The cyclic crack growth data could be fit to a Paris relationship between crack growth rate and stress intensity range. The stress intensity factor exponent, m, in the Paris relationship was between 4 and 6, which is comparable with the relatively high values found in the literature for the tension-tension fatigue of other metallic bulk materials. Incomplete self-similarity analysis was used to explain the observed higher m values for thin metallic foils. [PUBLICATION ABSTRACT] A low-cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular specimens. To illustrate the testing apparatus, mode I fatigue crack growth in 30- mu m-thick high-purity titanium foils was studied. Experiments were performed at ambient temperature using a loading frequency of 2 Hz and a nominal stress ratio of 0.1. The cyclic crack growth data could be fit to a Paris relationship between crack growth rate and stress intensity range. The stress intensity factor exponent, m, in the Paris relationship was between 4 and 6, which is comparable with the relatively high values found in the literature for the tension-tension fatigue of other metallic bulk materials. Incomplete self-similarity analysis was used to explain the observed higher m values for thin metallic foils. ABSTRACT A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular specimens. To illustrate the testing apparatus, mode I fatigue crack growth in 30‐µm‐thick high‐purity titanium foils was studied. Experiments were performed at ambient temperature using a loading frequency of 2 Hz and a nominal stress ratio of 0.1. The cyclic crack growth data could be fit to a Paris relationship between crack growth rate and stress intensity range. The stress intensity factor exponent, m , in the Paris relationship was between 4 and 6, which is comparable with the relatively high values found in the literature for the tension–tension fatigue of other metallic bulk materials. Incomplete self‐similarity analysis was used to explain the observed higher m values for thin metallic foils. ABSTRACT A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus utilizes magnetic coupling between a ceramic magnet and a rotating steel disc to induce cyclic tensile loads in notched rectangular specimens. To illustrate the testing apparatus, mode I fatigue crack growth in 30‐µm‐thick high‐purity titanium foils was studied. Experiments were performed at ambient temperature using a loading frequency of 2 Hz and a nominal stress ratio of 0.1. The cyclic crack growth data could be fit to a Paris relationship between crack growth rate and stress intensity range. The stress intensity factor exponent, m, in the Paris relationship was between 4 and 6, which is comparable with the relatively high values found in the literature for the tension–tension fatigue of other metallic bulk materials. Incomplete self‐similarity analysis was used to explain the observed higher m values for thin metallic foils. |
Author | Holmes, J. W. Liu, L. Lee, C.-W. |
Author_xml | – sequence: 1 givenname: C.-W. surname: Lee fullname: Lee, C.-W. organization: Department of Advanced Analysis and Characterization, Korea Institute of Materials Science, Changwon, South Korea – sequence: 2 givenname: L. surname: Liu fullname: Liu, L. email: liuliu@bit.edu.cn organization: School of Aerospace Engineering, Beijing Institute of Technology, 100081, Beijing, China – sequence: 3 givenname: J. W. surname: Holmes fullname: Holmes, J. W. organization: Center for Clean Energy Systems and Materials, Beihang University, 100191, Beijing, China |
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CitedBy_id | crossref_primary_10_1088_1361_6439_acddf3 crossref_primary_10_1016_j_ijfatigue_2017_01_046 crossref_primary_10_1016_j_ijfatigue_2018_05_009 crossref_primary_10_1016_j_msea_2018_01_039 crossref_primary_10_1016_j_engfailanal_2014_11_026 crossref_primary_10_1016_j_engfailanal_2023_107623 |
Cites_doi | 10.1023/A:1018655917051 10.1016/0013-7944(84)90123-1 10.1007/BF00040143 10.1016/S0921-5093(01)01249-7 10.1016/0013-7944(81)90039-4 10.7449/1991/Superalloys_1991_491_500 10.1016/j.actamat.2011.11.015 10.1016/j.msea.2007.02.132 10.1016/j.ijfatigue.2005.06.035 10.1023/A:1007630813025 10.1016/0013-7944(85)90109-2 10.1016/S0921-5093(01)01043-7 10.7449/2001/Superalloys_2001_669_678 10.1016/0921-5093(96)10226-4 10.1115/1.3609569 10.1016/j.msea.2011.04.046 10.1111/j.1460-2695.1980.tb01359.x 10.1007/s10704-005-2266-y 10.1023/B:FRAC.0000007376.06477.e8 10.1017/CBO9780511814921 10.1007/BF02643221 10.1016/j.msea.2006.03.090 10.1016/j.msea.2006.06.124 10.1115/1.2772324 |
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Keywords | Propagation velocity fatigue crack growth rate Growth titanium Mechanical properties Fatigue finite element analysis Modeling Fatigue crack Crack propagation Finite element method fatigue testing Thin sheet Development incomplete self-similarity Application |
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C. – volume-title: Standard Test Method for Measurement of Fatigue Crack Growth Rates year: 2008 ident: e_1_2_10_17_1 contributor: fullname: ASTM E 647‐08 – ident: e_1_2_10_34_1 doi: 10.1023/A:1018655917051 – ident: e_1_2_10_27_1 doi: 10.1016/0013-7944(84)90123-1 – volume: 2 start-page: 48 year: 1975 ident: e_1_2_10_32_1 article-title: A study of the fatigue crack growth at low temperatures publication-title: Physico‐Chem. Mech. Mater. contributor: fullname: Yarema S. Ya. – volume: 13 start-page: 267 year: 1977 ident: e_1_2_10_15_1 article-title: The essential work of plane stress ductile fracture publication-title: Inter. J. 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A low‐cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The... A low-cost experimental apparatus has been developed to investigate the mode I fatigue crack growth behaviour of thin metallic foils and sheets. The apparatus... |
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SubjectTerms | Applied sciences Crack propagation Exact sciences and technology Fatigue fatigue crack growth rate Fatigue failure fatigue testing finite element analysis Foils Foils (structural shapes) Fracture mechanics incomplete self-similarity Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metal fatigue Metals. Metallurgy Paris Stress intensity factors Testing equipment Titanium |
Title | Development of a fatigue crack growth testing apparatus and its application to thin titanium foil |
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