Materials Science, Vol. 47, No. 5It is shown that the deformation pattern is formed under cyclic loads and develops on the surface of the cladding layer of a structural aluminum alloy. The quantitative parameters of the deformation pattern, namely, the saturation, roughness, and plastic strains on the surface, serve as indicators of damage to the material. The experimental dependences of the analyzed parameters on the operating time (number of loading cycles) can be used for the creation of new methods aimed at the prediction of the limit state of structural elements of the aircraft structures
The possibility of atomic force microscopy application for the investigation of fatigue damage proce...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
The primary purpose of this report is to study how the surface properties of an aluminium alloy chan...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
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...
Advances in Military Technology, Vol. 8, No. 2, December 2013The possibility of fatigue damage analy...
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...
Durability and reliability of machines and mechanisms are determined, mainly, by their fatigue resis...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
The fatigue properties of thermo-mechanically treated and machined aluminum alloy 7475-T7351 have be...
The paper studies the effect of strain-loading sequence on fatigue lifetime and fracture surface top...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
The possibility of atomic force microscopy application for the investigation of fatigue damage proce...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
The primary purpose of this report is to study how the surface properties of an aluminium alloy chan...
International Journal of FatigueThe deformation relief was revealed to be formed and evolved on the ...
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...
Advances in Military Technology, Vol. 8, No. 2, December 2013The possibility of fatigue damage analy...
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...
Durability and reliability of machines and mechanisms are determined, mainly, by their fatigue resis...
Theoretical and Applied Fracture Mechanics, Volume 65It was shown by tests conducted at the National...
The fatigue properties of thermo-mechanically treated and machined aluminum alloy 7475-T7351 have be...
The paper studies the effect of strain-loading sequence on fatigue lifetime and fracture surface top...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
The characteristic informative parameters for defect detection to be used in fatigue sensors have be...
The possibility of atomic force microscopy application for the investigation of fatigue damage proce...
Aircraft are made primarily out of strong and lightweight aluminum alloys, which are relatively low ...
The primary purpose of this report is to study how the surface properties of an aluminium alloy chan...