Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/32283
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Karuskevich, M.V. | - |
dc.date.accessioned | 2017-12-26T12:45:12Z | - |
dc.date.available | 2017-12-26T12:45:12Z | - |
dc.date.issued | 2014 | - |
dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/32283 | - |
dc.description | Вісник НАУ, 2012, №1 | uk_UA |
dc.description.abstract | The investigations of the new fatigue sensor that was carried out at the wide range of cyclic loads conditions show the ability of the indicator application in Structural Health Monitoring systems of planes, bridges, vessels, and other structures. Accumulated fatigue damage may by estimated by the intensity of deformation relief, i.e. by its extrusion/intrusion and persistent slip bands structures on the indicator surface. | uk_UA |
dc.language.iso | en | uk_UA |
dc.publisher | Ніціональний авіаційний університет | uk_UA |
dc.subject | alclad aluminum alloys | uk_UA |
dc.subject | deformation relief | uk_UA |
dc.subject | fatigue | uk_UA |
dc.subject | fatigue indicator | uk_UA |
dc.title | Fatigue life prediction by the structurally sensitive damage indicator | uk_UA |
dc.type | Article | uk_UA |
dc.subject.udc | 620.179.1 | - |
dc.speciality | Reliability and durability | uk_UA |
Appears in Collections: | Статті в наукових виданнях кафедри конструкції літальних апаратів |
Files in This Item:
File | Description | Size | Format | |
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Sensor.pdf | Стаття | 3.73 MB | Adobe PDF | View/Open |
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