AbstractIn order to guarantee a fatigue lifetime with a conventional and low probability of failure, a probabilistic fatigue assessment diagram is proposed as a tool. The safe domain is limited by the fatigue failure assessment curve, which depends on material properties through Basquin's exponent, endurance limit and low cycle fatigue domain. From the double-truncated distribution of the targeted maximum applied stress, it is possible to find the failure probability and its associated safety factor. An example of an aeronautical component made of TA6V titanium alloy welded by laser and exhibiting an undercut at the weld toe is given
A methodology is presented for integrating probabilistic fracture mechanics with quantitative NDT fo...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
The use of predicted fatigue ctack growth bthavior in the updating of the fatigue design lifek inves...
Abstract In order to guarantee a fatigue lifetime with a conventional and low probability of failure...
AbstractIn order to guarantee a fatigue lifetime with a conventional and low probability of failure,...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
One of the most frequent and dangerous failure modes in continuous welded rails is fatigue crack pro...
The subject of this thesis is the probabilistic reliability assessment of notched metallic component...
Metal fatigue under stress and thermal cycling is a principal mode of failure in gas turbine engine ...
AbstractA probabilistic fracture mechanics model is applied to irradiation assisted stress corrosion...
Paper describes in detail and gives example of the probabilistic assessment of a steel structural el...
Abstract Probabilistic routines are necessary to determine the permissible design stress when the op...
AbstractThe aim of the present work is to develop a statistical approach for the correlation between...
Two series of low cycle fatigue (LCF) test data for two groups of different aircraft gas turbine eng...
Aerospace design requirements mandate acceptable levels of structural failure risk. Probabilistic f...
A methodology is presented for integrating probabilistic fracture mechanics with quantitative NDT fo...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
The use of predicted fatigue ctack growth bthavior in the updating of the fatigue design lifek inves...
Abstract In order to guarantee a fatigue lifetime with a conventional and low probability of failure...
AbstractIn order to guarantee a fatigue lifetime with a conventional and low probability of failure,...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
One of the most frequent and dangerous failure modes in continuous welded rails is fatigue crack pro...
The subject of this thesis is the probabilistic reliability assessment of notched metallic component...
Metal fatigue under stress and thermal cycling is a principal mode of failure in gas turbine engine ...
AbstractA probabilistic fracture mechanics model is applied to irradiation assisted stress corrosion...
Paper describes in detail and gives example of the probabilistic assessment of a steel structural el...
Abstract Probabilistic routines are necessary to determine the permissible design stress when the op...
AbstractThe aim of the present work is to develop a statistical approach for the correlation between...
Two series of low cycle fatigue (LCF) test data for two groups of different aircraft gas turbine eng...
Aerospace design requirements mandate acceptable levels of structural failure risk. Probabilistic f...
A methodology is presented for integrating probabilistic fracture mechanics with quantitative NDT fo...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
The use of predicted fatigue ctack growth bthavior in the updating of the fatigue design lifek inves...