AbstractThe influence of frequency (20kHz ultrasonic tests and conventional 20 to 35Hz tests) and environment (air and vacuum) on near-threshold fatigue crack propagation of three metallic alloys, Ti-6Al-4V, 2024-T351 and 12% Cr stainless steel is compared experimentally. The effective stress-intensity factor which is considered as the propagation driving force is determined from closure measurements or tests run at high R-ratio. Based on microfractographic observations, the results are discussed in terms of a preexisting model for intrinsic and environmentally assisted fatigue crack propagation
AbstractFatigue properties of age-hardened Al alloy 2017-T4 under ultrasonic loading frequency (20 k...
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
An enhanced life management system for aircraft turbine engine rotors based on probabilistic damage ...
AbstractThe existence or non-existence of fatigue crack growth thresholds is of practical importance...
AbstractFatigue crack propagation is studied in thin wires of about 1 mm in diameter of an ultra hig...
Investigations have shown that in the regime of Very High Cycle Fatigue (VHCF) “natural” crack initi...
ABSTRACT: This paper deals with a study on a perplexing phenomenon which has been recently reported ...
The definition of the critical levels of microstructural damage that can lead to the propagation of ...
International audienceIn this paper, the near-threshold fatigue behavior of physically through-thick...
AbstractThe principles of the ultrasonic 20 kHz technique are shortly described and its peculiaritie...
AbstractThe fatigue crack initiation mechanisms prevalent in high strength martensitic steel grades,...
To understand the influence temperature on the rate of fatigue crack growth in high strength metal a...
The loading frequency effects on elevated temperature fatigue crack growth behavior in a new near-α,...
AbstractNDT on-line monitoring methodology was applied at the servo-hydraulic machine to monitor the...
To determine the effects of vacuum environment on fatigue crack propagations in a Ti-6Al-4V alloy, K...
AbstractFatigue properties of age-hardened Al alloy 2017-T4 under ultrasonic loading frequency (20 k...
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
An enhanced life management system for aircraft turbine engine rotors based on probabilistic damage ...
AbstractThe existence or non-existence of fatigue crack growth thresholds is of practical importance...
AbstractFatigue crack propagation is studied in thin wires of about 1 mm in diameter of an ultra hig...
Investigations have shown that in the regime of Very High Cycle Fatigue (VHCF) “natural” crack initi...
ABSTRACT: This paper deals with a study on a perplexing phenomenon which has been recently reported ...
The definition of the critical levels of microstructural damage that can lead to the propagation of ...
International audienceIn this paper, the near-threshold fatigue behavior of physically through-thick...
AbstractThe principles of the ultrasonic 20 kHz technique are shortly described and its peculiaritie...
AbstractThe fatigue crack initiation mechanisms prevalent in high strength martensitic steel grades,...
To understand the influence temperature on the rate of fatigue crack growth in high strength metal a...
The loading frequency effects on elevated temperature fatigue crack growth behavior in a new near-α,...
AbstractNDT on-line monitoring methodology was applied at the servo-hydraulic machine to monitor the...
To determine the effects of vacuum environment on fatigue crack propagations in a Ti-6Al-4V alloy, K...
AbstractFatigue properties of age-hardened Al alloy 2017-T4 under ultrasonic loading frequency (20 k...
AbstractThe paper presents an experimental work of fatigue crack growth for aerospace 2024 T351 alum...
An enhanced life management system for aircraft turbine engine rotors based on probabilistic damage ...