This paper investigates the differences in the predicted fatigue life of transverse butt weld joints and cover-plated beams considering statistically based fitting methods on fatigue test data and comparing the results with the S-N relation proposed in international standards. The test data fitting are performed by employing the Least Square Method (LSM) and the Maximum Likelihood Method (MLM) taking into account the contribution of the runouts. The Mean curve, the characteristic curve and the design curve have been derived. In order to consider the effect of Variable Amplitude loading, the S-N curves have been extended and the fatigue damage according to the Palmgren-Miner cumulative damage rule is evaluated for a load spectrum that follow...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
An S-N curve is essential not only for describing fatigue results from tests for un-notched specimen...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
Reliability analysis is a crucial phase in assessing the safety status of new and existing structure...
Investigations of cumulative damage were carried out on two types of welded joints (butt welds and t...
Reliability analysis is a crucial phase in assessing the safety status of new and existing structure...
Reliability analysis is a crucial phase in assessing the safety status of new and existing structure...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
An S-N curve is essential not only for describing fatigue results from tests for un-notched specimen...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
This paper investigates the differences in the predicted fatigue life of transverse butt weld joints...
Reliability analysis is a crucial phase in assessing the safety status of new and existing structure...
Investigations of cumulative damage were carried out on two types of welded joints (butt welds and t...
Reliability analysis is a crucial phase in assessing the safety status of new and existing structure...
Reliability analysis is a crucial phase in assessing the safety status of new and existing structure...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
In design against fatigue, a lower bound stress range vs. endurance curve (S-N curve) is employed to...
An S-N curve is essential not only for describing fatigue results from tests for un-notched specimen...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...