Damage mechanics analysis for predicting mechanical behavior of general composite laminates containing transverse cracks.
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| Title: | Damage mechanics analysis for predicting mechanical behavior of general composite laminates containing transverse cracks. |
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| Authors: | Kobayashi, Satoshi, Ogihara, Shinji, Takeda, Nobuo |
| Source: | Advanced Composite Materials. 2000, Vol. 9 Issue 4, p363-375. 13p. |
| Subjects: | Laminated materials, Composite materials |
| Abstract: | A damage mechanics analysis is applied to predict the relation between laminate stress and strain in composite laminates containing transverse matrix cracks. First, the transverse crack density as a function of laminate stress is predicted based on both energy and average stress criteria. Next, the laminate strain increment caused by transverse cracking is also derived as a function of applied laminate stress and transverse crack density, and then the relation between laminate stress and strain is predicted considering matrix cracking. The analytical prediction of the relation between laminate stress and strain is compared with the experimental results. The analytical prediction slightly underestimates the laminate stress because the strain increment associated with transverse crack opening displacement is overestimated in this analysis. An advantage of the present method is that it can be applied to laminates with arbitrary stacking sequences. [ABSTRACT FROM AUTHOR] |
| Copyright of Advanced Composite Materials is the property of Taylor & Francis Ltd 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 | Links: – Type: pdflink Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 4948720 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Damage mechanics analysis for predicting mechanical behavior of general composite laminates containing transverse cracks. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Kobayashi%2C+Satoshi%22">Kobayashi, Satoshi</searchLink><br /><searchLink fieldCode="AR" term="%22Ogihara%2C+Shinji%22">Ogihara, Shinji</searchLink><br /><searchLink fieldCode="AR" term="%22Takeda%2C+Nobuo%22">Takeda, Nobuo</searchLink> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Advanced+Composite+Materials%22">Advanced Composite Materials</searchLink>. 2000, Vol. 9 Issue 4, p363-375. 13p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Laminated+materials%22">Laminated materials</searchLink><br /><searchLink fieldCode="DE" term="%22Composite+materials%22">Composite materials</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: A damage mechanics analysis is applied to predict the relation between laminate stress and strain in composite laminates containing transverse matrix cracks. First, the transverse crack density as a function of laminate stress is predicted based on both energy and average stress criteria. Next, the laminate strain increment caused by transverse cracking is also derived as a function of applied laminate stress and transverse crack density, and then the relation between laminate stress and strain is predicted considering matrix cracking. The analytical prediction of the relation between laminate stress and strain is compared with the experimental results. The analytical prediction slightly underestimates the laminate stress because the strain increment associated with transverse crack opening displacement is overestimated in this analysis. An advantage of the present method is that it can be applied to laminates with arbitrary stacking sequences. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of Advanced Composite Materials is the property of Taylor & Francis Ltd 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=4948720 |
| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1163/15685510052000165 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 13 StartPage: 363 Subjects: – SubjectFull: Laminated materials Type: general – SubjectFull: Composite materials Type: general Titles: – TitleFull: Damage mechanics analysis for predicting mechanical behavior of general composite laminates containing transverse cracks. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Kobayashi, Satoshi – PersonEntity: Name: NameFull: Ogihara, Shinji – PersonEntity: Name: NameFull: Takeda, Nobuo IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 12 Text: 2000 Type: published Y: 2000 Identifiers: – Type: issn-print Value: 09243046 Numbering: – Type: volume Value: 9 – Type: issue Value: 4 Titles: – TitleFull: Advanced Composite Materials Type: main |
| ResultId | 1 |
