AbstractThe theory of economic life prediction and reliability assessment of aircraft structures has a significant effect on safety of aircraft structures. It is based on the two-stage theory of fatigue process and can guarantee the safety and reliability of structures. According to the fatigue damage process, the fatigue scatter factors of crack initiation stage and crack propagation stage are given respectively. At the same time, mathematical models of fatigue life prediction are presented by utilizing the fatigue scatter factors and full scale test results of aircraft structures. Furthermore, the economic life model is put forward. The model is of significant scientific value for products to provide longer economic life, higher reliabili...
The concept of time to first failure is utilized to perform a parameter study of scatter factors of ...
A mechanical component can break due to repeated load cycling, even if these loads remain well below...
This work presents total fatigue life prediction methodology of aircraft structural components under...
Issued as Semi-annual report [1-4], and Final report, Project no. E-16-631Final report has title: Re...
Confront with the serious aging problem in aircraft structure field, the profession was tasked to un...
This paper outlines a new durability model to assess the first inspection and maintenance period for...
The fatigue life scatter factor is an important reliability index of the assessment of aircraft fati...
Fatigue is the mechanism of progressive damage which may ultimately limit the economic life of an ai...
In this paper, some progress and achievements in aircraft integrity requirements, structural health ...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...
This paper represents fatigue crack growth life prediction in thin-walled structures (plates or shel...
ABSTRACT: The lead crack concept is adopted as the basis for a new fatigue lifeing method using the ...
Fatigue performance of structures is greatly affected by the presence of stress raisers such as fast...
Fatigue failure of the airframe structure occurs almost in the hole position of the fastener hole,St...
Aircraft structure with holes was thought to have a significant impact towards fatigue life. Holes ...
The concept of time to first failure is utilized to perform a parameter study of scatter factors of ...
A mechanical component can break due to repeated load cycling, even if these loads remain well below...
This work presents total fatigue life prediction methodology of aircraft structural components under...
Issued as Semi-annual report [1-4], and Final report, Project no. E-16-631Final report has title: Re...
Confront with the serious aging problem in aircraft structure field, the profession was tasked to un...
This paper outlines a new durability model to assess the first inspection and maintenance period for...
The fatigue life scatter factor is an important reliability index of the assessment of aircraft fati...
Fatigue is the mechanism of progressive damage which may ultimately limit the economic life of an ai...
In this paper, some progress and achievements in aircraft integrity requirements, structural health ...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...
This paper represents fatigue crack growth life prediction in thin-walled structures (plates or shel...
ABSTRACT: The lead crack concept is adopted as the basis for a new fatigue lifeing method using the ...
Fatigue performance of structures is greatly affected by the presence of stress raisers such as fast...
Fatigue failure of the airframe structure occurs almost in the hole position of the fastener hole,St...
Aircraft structure with holes was thought to have a significant impact towards fatigue life. Holes ...
The concept of time to first failure is utilized to perform a parameter study of scatter factors of ...
A mechanical component can break due to repeated load cycling, even if these loads remain well below...
This work presents total fatigue life prediction methodology of aircraft structural components under...