Add to ORKGInternational Journal of FatigueThe deformation relief was revealed to be formed and evolved on the surface of a cladding layer of a D16AT aluminum alloy under random cyclic loading. The surface saturation, roughness, and microplastic deformation are found to be quantitative estimates of the deformation relief and damage levels. Experimental deformation relief characteristics-load cycle number relations are similar and can be employed for predicting the fatigue crack initiation in aircraft structure elements
Durability and reliability of machines and mechanisms are determined, mainly, by their fatigue resis...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
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 peculiarities of using the surface as a damage sensor of the A2024 aluminum alloy under signific...
The analysis of loading conditions of modern civil aircrafts, the existing methods for evaluation of...
International Journal of Fatigue 39 (2012)Two approaches to aircraft fatigue monitoring by the compu...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
The subject of the paper is the considerations of the capability of load-time history reconstruction...
Advances in Military Technology, Vol. 8, No. 2, December 2013The possibility of fatigue damage analy...
The paper studies the effect of strain-loading sequence on fatigue lifetime and fracture surface top...
Durability and reliability of machines and mechanisms are determined, mainly, by their fatigue resis...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
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 peculiarities of using the surface as a damage sensor of the A2024 aluminum alloy under signific...
The analysis of loading conditions of modern civil aircrafts, the existing methods for evaluation of...
International Journal of Fatigue 39 (2012)Two approaches to aircraft fatigue monitoring by the compu...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
The subject of the paper is the considerations of the capability of load-time history reconstruction...
Advances in Military Technology, Vol. 8, No. 2, December 2013The possibility of fatigue damage analy...
The paper studies the effect of strain-loading sequence on fatigue lifetime and fracture surface top...
Durability and reliability of machines and mechanisms are determined, mainly, by their fatigue resis...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
Fatigue data are generally derived under constant-amplitude loading conditions, but aircraft compone...