Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue
The paper describes the key principles and results of preliminary experiments aimed at the development of new technique for the fatigue life prediction under conditions of biaxial cyclic tension. The foundations of the method were developed early by the numerous tests with monitoring the process of...
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| Format: | Article |
| Language: | English |
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Gruppo Italiano Frattura
2016-10-01
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| Series: | Fracture and Structural Integrity |
| Subjects: | |
| Online Access: | http://www.gruppofrattura.it/pdf/rivista/numero38/numero_38_art_27.pdf |
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| author | M.V. Karuskevich S.R. Ignatovich Т.P. Maslak A. Menou P.О. Maruschak S.V. Panin F. Berto |
| author_facet | M.V. Karuskevich S.R. Ignatovich Т.P. Maslak A. Menou P.О. Maruschak S.V. Panin F. Berto |
| author_sort | M.V. Karuskevich |
| collection | DOAJ |
| description | The paper describes the key principles and results of preliminary experiments aimed at the development of new technique for the fatigue life prediction under conditions of biaxial cyclic tension. The foundations of the method were developed early by the numerous tests with monitoring the process of surface deformation relief formation, which is proved to be an indicator of accumulated fatigue damage under uniaxial fatigue. The employed phenomenon was early applied for the development of a family of uniaxial loading fatigue sensors. The formation of strain induced relief has been recently taken into consideration as a part of damage accumulation criteria under biaxial fatigue as well. The home-made testing machine has been designed to implement combined bending and torsion loading that simulates loads experienced by an aircraft wing skin. The experimental evidences on formation and evolution of the deformation relief revealed under conditions of combined loading, supports the proposed concept of biaxial fatigue sensor |
| format | Article |
| id | doaj-art-f85de80b27504fc18db43d059b95eef0 |
| institution | Kabale University |
| issn | 1971-8993 1971-8993 |
| language | English |
| publishDate | 2016-10-01 |
| publisher | Gruppo Italiano Frattura |
| record_format | Article |
| series | Fracture and Structural Integrity |
| spelling | doaj-art-f85de80b27504fc18db43d059b95eef02025-01-02T23:02:13ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89931971-89932016-10-01103819820410.3221/IGF-ESIS.38.27Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigueM.V. Karuskevich0S.R. Ignatovich1Т.P. Maslak2A. Menou 3P.О. Maruschak4S.V. Panin 5F. Berto 6National Aviation University,UkaineNational Aviation University,UkaineNational Aviation University,UkaineInternational Academy of Civil Aviation, Casablanca, MoroccTernopil National Ivan Pul’uj Technical University,UkraineInstitute of Strength Physics and Materials Sciences,RussiaUniversity of Padova,ItalyThe paper describes the key principles and results of preliminary experiments aimed at the development of new technique for the fatigue life prediction under conditions of biaxial cyclic tension. The foundations of the method were developed early by the numerous tests with monitoring the process of surface deformation relief formation, which is proved to be an indicator of accumulated fatigue damage under uniaxial fatigue. The employed phenomenon was early applied for the development of a family of uniaxial loading fatigue sensors. The formation of strain induced relief has been recently taken into consideration as a part of damage accumulation criteria under biaxial fatigue as well. The home-made testing machine has been designed to implement combined bending and torsion loading that simulates loads experienced by an aircraft wing skin. The experimental evidences on formation and evolution of the deformation relief revealed under conditions of combined loading, supports the proposed concept of biaxial fatigue sensorhttp://www.gruppofrattura.it/pdf/rivista/numero38/numero_38_art_27.pdfDefectsFatigue sensorsDamageAviation |
| spellingShingle | M.V. Karuskevich S.R. Ignatovich Т.P. Maslak A. Menou P.О. Maruschak S.V. Panin F. Berto Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue Fracture and Structural Integrity Defects Fatigue sensors Damage Aviation |
| title | Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue |
| title_full | Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue |
| title_fullStr | Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue |
| title_full_unstemmed | Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue |
| title_short | Multi-purpose fatigue sensor. Part 1. Uniaxial and multiaxial fatigue |
| title_sort | multi purpose fatigue sensor part 1 uniaxial and multiaxial fatigue |
| topic | Defects Fatigue sensors Damage Aviation |
| url | http://www.gruppofrattura.it/pdf/rivista/numero38/numero_38_art_27.pdf |
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