AbstractFatigue properties of age-hardened Al alloy 2017-T4 under ultrasonic loading frequency (20 kHz) were investigated and compared with the results under conventional loading of rotating bending (50 Hz). The growth of a crack retarded at about 500µm in surface length under ultrasonic loading, while at about 20µm under rotating bending. Although striations being a typical fracture mechanism were observed under conventional loading, most of fracture surface was covered with many facets under ultrasonic loading. These facets were also observed under rotating bending in nitrogen gas. The difference in growth mechanism depending on the loading frequency and the retardation of a crack growth under ultrasonic loading may be caused by the envir...
To understand the influence temperature on the rate of fatigue crack growth in high strength metal a...
AbstractA new ultrasonic fatigue testing device has been developed to test specimens under biaxial l...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
AbstractFatigue properties of age-hardened Al alloy 2017-T4 under ultrasonic loading frequency (20 k...
Improving fatigue life is one of the most important issues in mechanical design; an investigation ha...
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
AbstractUltrasonic fatigue testing allows time saving investigations up to the very high cycle fatig...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
Paper presents the “in situ” method for determining of irreversible fatigue damage accumulation, bas...
AbstractThe influence of frequency (20kHz ultrasonic tests and conventional 20 to 35Hz tests) and en...
Abstract Effect of humidity on the propagation mechanism of a fatigue crack in age-hardened Al alloy...
Investigations have shown that in the regime of Very High Cycle Fatigue (VHCF) “natural” crack initi...
In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plast...
In this paper we investigated the influence of consecutive dynamic and gigacycle fatigue loads on th...
AbstractThe principles of the ultrasonic 20 kHz technique are shortly described and its peculiaritie...
To understand the influence temperature on the rate of fatigue crack growth in high strength metal a...
AbstractA new ultrasonic fatigue testing device has been developed to test specimens under biaxial l...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...
AbstractFatigue properties of age-hardened Al alloy 2017-T4 under ultrasonic loading frequency (20 k...
Improving fatigue life is one of the most important issues in mechanical design; an investigation ha...
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
AbstractUltrasonic fatigue testing allows time saving investigations up to the very high cycle fatig...
AbstractThe present work is devoted to study the influence of high cycle fatigue damage rate at R = ...
Paper presents the “in situ” method for determining of irreversible fatigue damage accumulation, bas...
AbstractThe influence of frequency (20kHz ultrasonic tests and conventional 20 to 35Hz tests) and en...
Abstract Effect of humidity on the propagation mechanism of a fatigue crack in age-hardened Al alloy...
Investigations have shown that in the regime of Very High Cycle Fatigue (VHCF) “natural” crack initi...
In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plast...
In this paper we investigated the influence of consecutive dynamic and gigacycle fatigue loads on th...
AbstractThe principles of the ultrasonic 20 kHz technique are shortly described and its peculiaritie...
To understand the influence temperature on the rate of fatigue crack growth in high strength metal a...
AbstractA new ultrasonic fatigue testing device has been developed to test specimens under biaxial l...
AbstractAluminium alloys of the 7000 series are largely used in aeronautical structural applications...