Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios
Because of good crack growth resistance owe to the fibers between the aluminum layers, fiber metal laminates (FML) offer significant improvements compared to currently applied materials for aircraft structures. The crack resistance of different reinforced fibers, glass fiber, and carbon fiber, under...
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| Published in: | Проблемы прочности |
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| Date: | 2016 |
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| Format: | Article |
| Language: | English |
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Інститут проблем міцності ім. Г.С. Писаренко НАН України
2016
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| Online Access: | https://nasplib.isofts.kiev.ua/handle/123456789/173427 |
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| Journal Title: | Digital Library of Periodicals of National Academy of Sciences of Ukraine |
| Cite this: | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios / X. Song, Z.Y. Li, Y. Shen, Y.L. Chen, J.Z. Zhang // Проблемы прочности. — 2016. — № 1. — С. 138-144. — Бібліогр.: 9 назв. — англ. |
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Digital Library of Periodicals of National Academy of Sciences of Ukraine| _version_ | 1862590409266429952 |
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| author | Song, X. Li, Z.Y Shen, Y. Chen, Y.L. Zhang, J.Z. |
| author_facet | Song, X. Li, Z.Y Shen, Y. Chen, Y.L. Zhang, J.Z. |
| citation_txt | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios / X. Song, Z.Y. Li, Y. Shen, Y.L. Chen, J.Z. Zhang // Проблемы прочности. — 2016. — № 1. — С. 138-144. — Бібліогр.: 9 назв. — англ. |
| collection | DSpace DC |
| container_title | Проблемы прочности |
| description | Because of good crack growth resistance owe to the fibers between the aluminum layers, fiber metal laminates (FML) offer significant improvements compared to currently applied materials for aircraft structures. The crack resistance of different reinforced fibers, glass fiber, and carbon fiber, under stress ratio R = -1, 0.1, and 0.5, respectively, are analyzed through test data. The results showed significant scatter in the positive stress ratio and obvious difference between two outer aluminum layers. So, the failure criterions of metal materials specified in the test standard are unsuitable for the FMLs fatigue test, and it is a problem to determine the failure criterion according to the engineering applications. This study is an experimental investigations with respect to the FMLs crack resistance and a qualitative conclusions have been drawn from the data analysis.
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| first_indexed | 2025-11-27T04:48:43Z |
| format | Article |
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| id | nasplib_isofts_kiev_ua-123456789-173427 |
| institution | Digital Library of Periodicals of National Academy of Sciences of Ukraine |
| issn | 0556-171X |
| language | English |
| last_indexed | 2025-11-27T04:48:43Z |
| publishDate | 2016 |
| publisher | Інститут проблем міцності ім. Г.С. Писаренко НАН України |
| record_format | dspace |
| spelling | Song, X. Li, Z.Y Shen, Y. Chen, Y.L. Zhang, J.Z. 2020-12-03T20:58:31Z 2020-12-03T20:58:31Z 2016 Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios / X. Song, Z.Y. Li, Y. Shen, Y.L. Chen, J.Z. Zhang // Проблемы прочности. — 2016. — № 1. — С. 138-144. — Бібліогр.: 9 назв. — англ. 0556-171X https://nasplib.isofts.kiev.ua/handle/123456789/173427 539.4 Because of good crack growth resistance owe to the fibers between the aluminum layers, fiber metal laminates (FML) offer significant improvements compared to currently applied materials for aircraft structures. The crack resistance of different reinforced fibers, glass fiber, and carbon fiber, under stress ratio R = -1, 0.1, and 0.5, respectively, are analyzed through test data. The results showed significant scatter in the positive stress ratio and obvious difference between two outer aluminum layers. So, the failure criterions of metal materials specified in the test standard are unsuitable for the FMLs fatigue test, and it is a problem to determine the failure criterion according to the engineering applications. This study is an experimental investigations with respect to the FMLs crack resistance and a qualitative conclusions have been drawn from the data analysis. The work was supported by the National Nature Science Foundation of China under the Contract No. 51271067. en Інститут проблем міцності ім. Г.С. Писаренко НАН України Проблемы прочности Научно-технический раздел Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios Сравнительный анализ трещиностойкости металловолоконных многослойных материалов со слоями стекла HS2 и углерода Т700 при различных коэффициентах асимметрии цикла Article published earlier |
| spellingShingle | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios Song, X. Li, Z.Y Shen, Y. Chen, Y.L. Zhang, J.Z. Научно-технический раздел |
| title | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios |
| title_alt | Сравнительный анализ трещиностойкости металловолоконных многослойных материалов со слоями стекла HS2 и углерода Т700 при различных коэффициентах асимметрии цикла |
| title_full | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios |
| title_fullStr | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios |
| title_full_unstemmed | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios |
| title_short | Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios |
| title_sort | comparative analysis of crack resistance of fiber metal laminates with hs2 glass/t700 carbon layers for various stress ratios |
| topic | Научно-технический раздел |
| topic_facet | Научно-технический раздел |
| url | https://nasplib.isofts.kiev.ua/handle/123456789/173427 |
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