Approximate determination of a strain-controlled fatigue life curve for aluminum alloy sheets for aircraft structures
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| Title: | Approximate determination of a strain-controlled fatigue life curve for aluminum alloy sheets for aircraft structures |
|---|---|
| Authors: | Lipski, Adam adam.lipski@utp.edu.pl, Mroziński, Stanisław1 |
| Source: | International Journal of Fatigue. Jun2012, Vol. 39, p2-7. 6p. |
| Subjects: | Aluminum alloy fatigue, Approximation theory, Strains & stresses (Mechanics), Airframes, Numerical calculations, Curves |
| Abstract: | Abstract: This paper deals with selected methods of approximate determination of a strain-controlled fatigue life curve for aluminum alloy sheets used in aircraft structures. Authors based their analysis of those methods on the results of own research of 2024-T3 alloy and its Russian equivalent D16CzATW. The approximate strain-fatigue life curves were compared with the experimental curves. The influence of inconsistencies between those curves on the calculation results was analyzed on computational examples by means of the Palmgren–Miner’s rule. [Copyright &y& Elsevier] |
| Copyright of International Journal of Fatigue is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | Engineering Source |
| FullText | Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 71804969 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Approximate determination of a strain-controlled fatigue life curve for aluminum alloy sheets for aircraft structures – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Lipski%2C+Adam%22">Lipski, Adam</searchLink><i> adam.lipski@utp.edu.pl</i><br /><searchLink fieldCode="AR" term="%22Mroziński%2C+Stanisław%22">Mroziński, Stanisław</searchLink><relatesTo>1</relatesTo> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22International+Journal+of+Fatigue%22">International Journal of Fatigue</searchLink>. Jun2012, Vol. 39, p2-7. 6p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Aluminum+alloy+fatigue%22">Aluminum alloy fatigue</searchLink><br /><searchLink fieldCode="DE" term="%22Approximation+theory%22">Approximation theory</searchLink><br /><searchLink fieldCode="DE" term="%22Strains+%26+stresses+%28Mechanics%29%22">Strains & stresses (Mechanics)</searchLink><br /><searchLink fieldCode="DE" term="%22Airframes%22">Airframes</searchLink><br /><searchLink fieldCode="DE" term="%22Numerical+calculations%22">Numerical calculations</searchLink><br /><searchLink fieldCode="DE" term="%22Curves%22">Curves</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: Abstract: This paper deals with selected methods of approximate determination of a strain-controlled fatigue life curve for aluminum alloy sheets used in aircraft structures. Authors based their analysis of those methods on the results of own research of 2024-T3 alloy and its Russian equivalent D16CzATW. The approximate strain-fatigue life curves were compared with the experimental curves. The influence of inconsistencies between those curves on the calculation results was analyzed on computational examples by means of the Palmgren–Miner’s rule. [Copyright &y& Elsevier] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of International Journal of Fatigue is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
| PLink | https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=egs&AN=71804969 |
| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1016/j.ijfatigue.2011.08.007 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 6 StartPage: 2 Subjects: – SubjectFull: Aluminum alloy fatigue Type: general – SubjectFull: Approximation theory Type: general – SubjectFull: Strains & stresses (Mechanics) Type: general – SubjectFull: Airframes Type: general – SubjectFull: Numerical calculations Type: general – SubjectFull: Curves Type: general Titles: – TitleFull: Approximate determination of a strain-controlled fatigue life curve for aluminum alloy sheets for aircraft structures Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Lipski, Adam – PersonEntity: Name: NameFull: Mroziński, Stanisław IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 06 Text: Jun2012 Type: published Y: 2012 Identifiers: – Type: issn-print Value: 01421123 Numbering: – Type: volume Value: 39 Titles: – TitleFull: International Journal of Fatigue Type: main |
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