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...
Збережено в:
| Дата: | 2016 |
|---|---|
| Автори: | , , , , |
| Формат: | Стаття |
| Мова: | English |
| Опубліковано: |
Інститут проблем міцності ім. Г.С. Писаренко НАН України
2016
|
| Назва видання: | Проблемы прочности |
| Теми: | |
| Онлайн доступ: | http://dspace.nbuv.gov.ua/handle/123456789/173427 |
| Теги: |
Додати тег
Немає тегів, Будьте першим, хто поставить тег для цього запису!
|
| Назва журналу: | Digital Library of Periodicals of National Academy of Sciences of Ukraine |
| Цитувати: | 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. |
Репозитарії
Digital Library of Periodicals of National Academy of Sciences of Ukraine| id |
irk-123456789-173427 |
|---|---|
| record_format |
dspace |
| spelling |
irk-123456789-1734272020-12-04T01:26:42Z 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 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. 2016 Article 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 http://dspace.nbuv.gov.ua/handle/123456789/173427 539.4 en Проблемы прочности Інститут проблем міцності ім. Г.С. Писаренко НАН України |
| institution |
Digital Library of Periodicals of National Academy of Sciences of Ukraine |
| collection |
DSpace DC |
| language |
English |
| topic |
Научно-технический раздел Научно-технический раздел |
| spellingShingle |
Научно-технический раздел Научно-технический раздел Song, X. Li, Z.Y Shen, Y. Chen, Y.L. Zhang, J.Z. Comparative Analysis of Crack Resistance of Fiber Metal Laminates with HS2 Glass/T700 Carbon Layers for Various Stress Ratios 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. |
| format |
Article |
| 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. |
| author_sort |
Song, X. |
| title |
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_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_sort |
comparative analysis of crack resistance of fiber metal laminates with hs2 glass/t700 carbon layers for various stress ratios |
| publisher |
Інститут проблем міцності ім. Г.С. Писаренко НАН України |
| publishDate |
2016 |
| topic_facet |
Научно-технический раздел |
| url |
http://dspace.nbuv.gov.ua/handle/123456789/173427 |
| 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. |
| series |
Проблемы прочности |
| work_keys_str_mv |
AT songx comparativeanalysisofcrackresistanceoffibermetallaminateswithhs2glasst700carbonlayersforvariousstressratios AT lizy comparativeanalysisofcrackresistanceoffibermetallaminateswithhs2glasst700carbonlayersforvariousstressratios AT sheny comparativeanalysisofcrackresistanceoffibermetallaminateswithhs2glasst700carbonlayersforvariousstressratios AT chenyl comparativeanalysisofcrackresistanceoffibermetallaminateswithhs2glasst700carbonlayersforvariousstressratios AT zhangjz comparativeanalysisofcrackresistanceoffibermetallaminateswithhs2glasst700carbonlayersforvariousstressratios |
| first_indexed |
2023-10-18T22:34:05Z |
| last_indexed |
2023-10-18T22:34:05Z |
| _version_ |
1796155855919382528 |