Add to ORKGIn many engineering structures measures to improve the fatigue strength are used. Due to the fact that aircraft structures have to be extremly hight weight these technics are widely used in aircraft. The most frequent technics are explained in their effect on life to failure and in one case also in their effect on crack propagation
This project involved development of a method to predict the fatigue crack propagation process in th...
The analytical and experimental researches concerning predicting of fatigue crack growth in the ope...
This subject is connected with the structural health monitoring (SHM) of aircraft. Progressive metho...
Die Materialermüdung einer Flugzeugzelle ist ein kritischer Bereich für die Sicherheit eines Flugzeu...
The study has been intended to determine the most essential mechanical and fatigue properties as wel...
Failures can be broadly classified into two categories, those involving fracture and those without f...
Surface treatments improve the structural fatigue strength of metallic components. The degree of imp...
Early airplanes were designed using purely static conditions and mainly tested only based on simple ...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
EP 1902812 A1 UPAB: 20080519 NOVELTY - Metal components for aircraft are made up of metal sheets (1,...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
Material fatigue is the basic factor limiting aircraft's durability. It comes from the fact that cha...
Materials used in aircraft structures have (should have) certificates confirming their quality. Nowa...
In this paper there are some results of the European project AISHA. The project aim is the aircraft ...
This project involved development of a method to predict the fatigue crack propagation process in th...
The analytical and experimental researches concerning predicting of fatigue crack growth in the ope...
This subject is connected with the structural health monitoring (SHM) of aircraft. Progressive metho...
Die Materialermüdung einer Flugzeugzelle ist ein kritischer Bereich für die Sicherheit eines Flugzeu...
The study has been intended to determine the most essential mechanical and fatigue properties as wel...
Failures can be broadly classified into two categories, those involving fracture and those without f...
Surface treatments improve the structural fatigue strength of metallic components. The degree of imp...
Early airplanes were designed using purely static conditions and mainly tested only based on simple ...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
In the calculation of the dimensions of modern machines and building constructions, account is taken...
EP 1902812 A1 UPAB: 20080519 NOVELTY - Metal components for aircraft are made up of metal sheets (1,...
The publications on fracture of metals emphasize the importance of avoiding so far as possible al...
Material fatigue is the basic factor limiting aircraft's durability. It comes from the fact that cha...
Materials used in aircraft structures have (should have) certificates confirming their quality. Nowa...
In this paper there are some results of the European project AISHA. The project aim is the aircraft ...
This project involved development of a method to predict the fatigue crack propagation process in th...
The analytical and experimental researches concerning predicting of fatigue crack growth in the ope...
This subject is connected with the structural health monitoring (SHM) of aircraft. Progressive metho...