Fatigue cracks growth features in aluminum alloy D16AT
| dc.contributor.author | Ignatovich, S.R. | |
| dc.contributor.author | Krasnopolskii, V.S. | |
| dc.date.accessioned | 2017-10-14T11:09:04Z | |
| dc.date.available | 2017-10-14T11:09:04Z | |
| dc.date.issued | 2016 | |
| dc.description | Конгресс Авіація в 21 ст., Безпека авіації та космічні технології | uk_UA |
| dc.description.abstract | This paper investigates the description of the fatigue cracks growth in sheet aluminum alloy D16AT by exponential dependence. The results show that the propagation of all investigated fatigue cracks can be satisfactorily described by this dependence with grate values of the determination coefficient. | uk_UA |
| dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/30706 | |
| dc.language.iso | en | uk_UA |
| dc.speciality | Fatigue and fracture of aircraft structures | uk_UA |
| dc.subject.udc | 629.7.023:539.421(045) | |
| dc.title | Fatigue cracks growth features in aluminum alloy D16AT | uk_UA |
| dc.type | Article | uk_UA |
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