The paper ‘The effect of secondary metalworking processes on susceptibility of aircraft to catastrophic failures and prevention methods’ [1] emphasizes that fatigue is the main failure mode for metallic aircraft structures. This is corroborated by Figure 1 [2,3] and other sources [4-6]. (...) The discussions and comments in the following sections of the present document are directed to the foregoing statements and their validities
Aero-engines are critical components whose reliable performance decides the primary safety of an air...
In this paper we hypothesize that pitting corrosion can alter the location of fatigue failures in ai...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
Failures can be broadly classified into two categories, those involving fracture and those without f...
Despite many enquiries held as the result of accidents that occured to welded structures, publicatio...
The international technical experts in the areas of durability and damage tolerance of metallic airf...
In the few minutes we have left before adjourning this session, I\u27d like to review briefly variou...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
The Second International Symposium of Fatigue of Materials: Advances and Emergences in Understanding...
Il été prouvée dans plusieurs études de la littérature que la taille d'un composant affecte sa tenue...
Fatigue crack propagation (FCP) can be affected by environment in a variety of ways, each of which m...
This paper is devoted to a discussion and solution of the following problems: Determination of mean ...
The article describes theoretical studies of the influence of vibration frequency on the development...
There is an increasing acknowledgement in the engineering community that the response to this challe...
International technical experts in durability and damage tolerance of metallic airframe structures w...
Aero-engines are critical components whose reliable performance decides the primary safety of an air...
In this paper we hypothesize that pitting corrosion can alter the location of fatigue failures in ai...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...
Failures can be broadly classified into two categories, those involving fracture and those without f...
Despite many enquiries held as the result of accidents that occured to welded structures, publicatio...
The international technical experts in the areas of durability and damage tolerance of metallic airf...
In the few minutes we have left before adjourning this session, I\u27d like to review briefly variou...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
The Second International Symposium of Fatigue of Materials: Advances and Emergences in Understanding...
Il été prouvée dans plusieurs études de la littérature que la taille d'un composant affecte sa tenue...
Fatigue crack propagation (FCP) can be affected by environment in a variety of ways, each of which m...
This paper is devoted to a discussion and solution of the following problems: Determination of mean ...
The article describes theoretical studies of the influence of vibration frequency on the development...
There is an increasing acknowledgement in the engineering community that the response to this challe...
International technical experts in durability and damage tolerance of metallic airframe structures w...
Aero-engines are critical components whose reliable performance decides the primary safety of an air...
In this paper we hypothesize that pitting corrosion can alter the location of fatigue failures in ai...
Corrosion has been and still is a worldwide problem today. Not only has it cost governments and comp...