Please use this identifier to cite or link to this item:
https://er.nau.edu.ua/handle/NAU/31969
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Petrasek, M. | - |
dc.contributor.author | Ignatovich, S. R. | - |
dc.contributor.author | Karuskevich, M. V. | - |
dc.contributor.author | Maslak, T. P. | - |
dc.date.accessioned | 2017-12-17T17:42:18Z | - |
dc.date.available | 2017-12-17T17:42:18Z | - |
dc.date.issued | 2013-12 | - |
dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/31969 | - |
dc.description | Advances in Military Technology, Vol. 8, No. 2, December 2013 | uk_UA |
dc.description.abstract | The possibility of fatigue damage analysis by the extrusion/intrusion structures on the surface of aluminium alloy is shown. Quantitative characteristics of the extrusion/intrusion structures and the methods for their monitoring are substantiated. Two approaches for fatigue analysis are presented: a) direct inspection of the aircraft components, b) application of fatigue sensors. | uk_UA |
dc.language.iso | en | uk_UA |
dc.publisher | University of Defence | uk_UA |
dc.subject | aircraft | uk_UA |
dc.subject | fatigue | uk_UA |
dc.subject | alclad alloy | uk_UA |
dc.subject | deformation relief | uk_UA |
dc.subject | fatigue sensor | uk_UA |
dc.subject | structural health monitoring | uk_UA |
dc.title | Surface of metal as an indicator of fatigue damage | uk_UA |
dc.type | Article | uk_UA |
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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Petrasek.pdf | Статья | 4.08 MB | Adobe PDF | View/Open |
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