Add to ORKGAdvances in Military Technology, Vol. 8, No. 2, December 2013The 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
Despite the prevalence of fatigue and fatigue related failures little is known about the actual mech...
17th European Conference on fractureThe results of numerous tests show that quantitative estimation ...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
International Journal of Fatigue 39 (2012)Two approaches to aircraft fatigue monitoring by the compu...
The analysis of loading conditions of modern civil aircrafts, the existing methods for evaluation of...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
Materials Science, Vol. 47, No. 5It is shown that the deformation pattern is formed under cyclic loa...
The paper presents experimental results directed on the development of new empirical criterion for m...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
The aim of this study was to investigate the failure mechanism of riveted aluminium lap joints when ...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
Les alliages d'aluminium utilisés dans les structures aéronautiques (fuselage, voilure) sont soumis ...
The peculiarities of using the surface as a damage sensor of the A2024 aluminum alloy under signific...
Fatigue Fracture Engineering Material Structure, Vol. 15, No. 12The possibility of using specially p...
Despite the prevalence of fatigue and fatigue related failures little is known about the actual mech...
17th European Conference on fractureThe results of numerous tests show that quantitative estimation ...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
International Journal of Fatigue 39 (2012)Two approaches to aircraft fatigue monitoring by the compu...
The analysis of loading conditions of modern civil aircrafts, the existing methods for evaluation of...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
Materials Science, Vol. 47, No. 5It is shown that the deformation pattern is formed under cyclic loa...
The paper presents experimental results directed on the development of new empirical criterion for m...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
The aim of this study was to investigate the failure mechanism of riveted aluminium lap joints when ...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
Les alliages d'aluminium utilisés dans les structures aéronautiques (fuselage, voilure) sont soumis ...
The peculiarities of using the surface as a damage sensor of the A2024 aluminum alloy under signific...
Fatigue Fracture Engineering Material Structure, Vol. 15, No. 12The possibility of using specially p...
Despite the prevalence of fatigue and fatigue related failures little is known about the actual mech...
17th European Conference on fractureThe results of numerous tests show that quantitative estimation ...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...