This work describes the results of the experience acquired by the authors during their participation to some among the European research programs with the aim to develop a probabilistic risk assessment procedure to analyse the spreading of fatigue-induced damage in typical aeronautical components. The several steps of the procedure are pointed out, and especially the modeling of the damage evolutionary process; the initiation and the transitional probabilities, which characterize the passage from one damage level to a higher one, are fully characterized and their dependence from time and from the damage state of surrounding zones illustrated by various example results
The presence of rare metallurgical or manufacturing anomalies in aircraft turbine rotors/disks may c...
This thesis presents a new modeling framework and application methodology for the study of aircraft...
The paper has been intended to introduce a probabilistic method to estimate – from the standpoint of...
This work describes the results of the experience acquired by the authors during their participation...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
The accurate assessment of aircraft structure damage risk is the premise of establishing reasonable,...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
This paper presents an overview of the achievements of a research and development project sponsore...
AbstractIn order to meet the airworthiness requirements (FAR33.70) of large commercial aero-engines,...
Aircraft structural risk and reliability analysis has gained considerable interest in the area of ai...
Fatigue is the mechanism of progressive damage which may ultimately limit the economic life of an ai...
Current Federal Aviation Administration (FAA) rotor design certification practices risk assessment u...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
Intermittent non-destructive inspection has been used since long time for checking the integrity of ...
Impact on composite structures shows a different damage behaviour compared to metal structures. Due ...
The presence of rare metallurgical or manufacturing anomalies in aircraft turbine rotors/disks may c...
This thesis presents a new modeling framework and application methodology for the study of aircraft...
The paper has been intended to introduce a probabilistic method to estimate – from the standpoint of...
This work describes the results of the experience acquired by the authors during their participation...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
The accurate assessment of aircraft structure damage risk is the premise of establishing reasonable,...
This paper describes a new possible approach to fatigue design of aerospace components founded on pr...
This paper presents an overview of the achievements of a research and development project sponsore...
AbstractIn order to meet the airworthiness requirements (FAR33.70) of large commercial aero-engines,...
Aircraft structural risk and reliability analysis has gained considerable interest in the area of ai...
Fatigue is the mechanism of progressive damage which may ultimately limit the economic life of an ai...
Current Federal Aviation Administration (FAA) rotor design certification practices risk assessment u...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
Intermittent non-destructive inspection has been used since long time for checking the integrity of ...
Impact on composite structures shows a different damage behaviour compared to metal structures. Due ...
The presence of rare metallurgical or manufacturing anomalies in aircraft turbine rotors/disks may c...
This thesis presents a new modeling framework and application methodology for the study of aircraft...
The paper has been intended to introduce a probabilistic method to estimate – from the standpoint of...