Abstract Probabilistic routines are necessary to determine the permissible design stress when the operational conditions of traditional gas turbines are further challenged to reach higher performances in terms of flexibility. This paper focuses on the definition of a probabilistic tool aimed to simulate the damage development under combined high and low cycle fatigue conditions considering the stochastic nature of some of the variables introduced in the model. The variables considered in the present study are the long crack threshold Δ K th , LC and the slope of the crack growth law C in the so-called Paris region, the endurance limit Δ σ w 0 and the variability of the applied stress as it cannot be considered a fixed variable in the comple...
This report describes a formal method to quantify structural damage tolerance and reliability in the...
Fatigue assessment for gas turbine blades under combined high and low fatigue cyclic loading is very...
Due to intermittent renewable energy share, precise lifetime assessment procedures are necessary to ...
Probabilistic routines are necessary to determine the permissible design stress when the operational...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
Structural integrity is a vitally important field of engineering with fracture and fatigue causing t...
Metal fatigue under stress and thermal cycling is a principal mode of failure in gas turbine engine ...
Rotor discs for gas turbines are heavy components usually designed following a safe-life approach, w...
Turbine engine disk life prediction and understanding the associated risk remains a significant chal...
Gas turbine discs are heavily loaded due to centrifugal and thermal loads and are therefore designed...
AbstractIn order to guarantee a fatigue lifetime with a conventional and low probability of failure,...
Abstract In order to guarantee a fatigue lifetime with a conventional and low probability of failure...
In probabilistic design of materials for fracture-critical components in modern military turbine eng...
This report describes a formal method to quantify structural damage tolerance and reliability in the...
Fatigue assessment for gas turbine blades under combined high and low fatigue cyclic loading is very...
Due to intermittent renewable energy share, precise lifetime assessment procedures are necessary to ...
Probabilistic routines are necessary to determine the permissible design stress when the operational...
Maintaining the component service life beyond its historical limits requires the ability to accurate...
Structural integrity is a vitally important field of engineering with fracture and fatigue causing t...
Metal fatigue under stress and thermal cycling is a principal mode of failure in gas turbine engine ...
Rotor discs for gas turbines are heavy components usually designed following a safe-life approach, w...
Turbine engine disk life prediction and understanding the associated risk remains a significant chal...
Gas turbine discs are heavily loaded due to centrifugal and thermal loads and are therefore designed...
AbstractIn order to guarantee a fatigue lifetime with a conventional and low probability of failure,...
Abstract In order to guarantee a fatigue lifetime with a conventional and low probability of failure...
In probabilistic design of materials for fracture-critical components in modern military turbine eng...
This report describes a formal method to quantify structural damage tolerance and reliability in the...
Fatigue assessment for gas turbine blades under combined high and low fatigue cyclic loading is very...
Due to intermittent renewable energy share, precise lifetime assessment procedures are necessary to ...