Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/30706Full metadata record
| DC Field | Value | Language |
|---|---|---|
| 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.identifier.uri | http://er.nau.edu.ua/handle/NAU/30706 | - |
| 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.language.iso | en | uk_UA |
| dc.title | Fatigue cracks growth features in aluminum alloy D16AT | uk_UA |
| dc.type | Article | uk_UA |
| dc.subject.udc | 629.7.023:539.421(045) | - |
| dc.speciality | Fatigue and fracture of aircraft structures | uk_UA |
| Appears in Collections: | Матеріали конференцій кафедри конструкції літальних апаратів | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Fatigue cracks growth features in aluminum alloy D16AT.pdf | Доклад на конференции | 108.11 kB | Adobe PDF | View/Open |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.