Add to ORKGThe characteristic informative parameters for defect detection to be used in fatigue sensors have been established. Their development is interpreted in terms of scale levels of deformation and fracture. Damage accumulation of the sensor’s surface tends to exhibit the self-organization nature. It is accompanied by formation of "folded" strain-induced relief on the surface. The mechanisms of damage accumulation under cyclic deformation were analyzed with the use of the multiscale approach. KEYWORDS. Defects; Fatigue sensors; Damage; Aviation
This paper deals with the basic mechanisms of fatigue damage in materials exposed to service and a s...
The article presents two distinct measures for fatigue damage detection in additively manufactured ...
In real life production of dynamically loaded components, we might accept the risk of defects only i...
Frattura ed Integrità Strutturale, Issue 38 (2016);The paper describes the key principles and result...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
The paper describes the key principles and results of preliminary experiments aimed at the developme...
The analysis of loading conditions of modern civil aircrafts, the existing methods for evaluation of...
Advances in Military Technology, Vol. 8, No. 2, December 2013The possibility of fatigue damage analy...
The peculiarities of using the surface as a damage sensor of the A2024 aluminum alloy under signific...
International Journal of Fatigue 39 (2012)Two approaches to aircraft fatigue monitoring by the compu...
Optoelectronics, instrumentation and data processing, Vol. 50 No. 4, 2014Digital identification and ...
The paper presents experimental results directed on the development of new empirical criterion for m...
Materials Science, Vol. 47, No. 5It is shown that the deformation pattern is formed under cyclic loa...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
The aim of this study was to investigate the failure mechanism of riveted aluminium lap joints when ...
This paper deals with the basic mechanisms of fatigue damage in materials exposed to service and a s...
The article presents two distinct measures for fatigue damage detection in additively manufactured ...
In real life production of dynamically loaded components, we might accept the risk of defects only i...
Frattura ed Integrità Strutturale, Issue 38 (2016);The paper describes the key principles and result...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
The paper describes the key principles and results of preliminary experiments aimed at the developme...
The analysis of loading conditions of modern civil aircrafts, the existing methods for evaluation of...
Advances in Military Technology, Vol. 8, No. 2, December 2013The possibility of fatigue damage analy...
The peculiarities of using the surface as a damage sensor of the A2024 aluminum alloy under signific...
International Journal of Fatigue 39 (2012)Two approaches to aircraft fatigue monitoring by the compu...
Optoelectronics, instrumentation and data processing, Vol. 50 No. 4, 2014Digital identification and ...
The paper presents experimental results directed on the development of new empirical criterion for m...
Materials Science, Vol. 47, No. 5It is shown that the deformation pattern is formed under cyclic loa...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
The aim of this study was to investigate the failure mechanism of riveted aluminium lap joints when ...
This paper deals with the basic mechanisms of fatigue damage in materials exposed to service and a s...
The article presents two distinct measures for fatigue damage detection in additively manufactured ...
In real life production of dynamically loaded components, we might accept the risk of defects only i...