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The causes that had originated the failure (superficial cracks, geometric concentrator, abrupt change of thickness) have been studied, verifying, by means of the simplified evaluation procedure of fatigue life of the "Germanischer Lloyd" (GL) standard, that these causes can explain the failure detected in the period of time in which it happened.
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The influence of welding procedure on fatigue properties of gas tungsten arc welded (GTAW AISII 304L load carrying cruciform joints, containing lack of penetration (LOP) has been studied using a crack initiation propagation (I-P) method.
The result of proposed procedure is distribution function of fatigue lifetime which takes into account the complex geometry of the designed part and random character of the complex loading (multiaxial stress state) in a hotspot.
In this paper a design procedure for fatigue assessment of welded pipe penetrations in plated structures is presented.
In this paper, a procedure for fatigue analysis of a general wide-band stationary Gaussian process is developed in the frequency domain using a trimodal spectral formulation, based on a generalization of the principle proposed by Jiao and Moan for predicting bimodal fatigue damage.
Therefore, the focus is on a new short-time procedure for fatigue life calculation of composites based on several cyclic load increase tests of each laminate.
This paper describes the formulation and numerical implementation of an incremental procedure for fatigue crack growth simulation applied to three-dimensional thermoelasticity using the dual boundary element method.
The article at the end illustrates the application of the analytic procedure for fatigue lifetime prediction that combines fracture mechanics and the load redistribution model for determination of S N curve parameters important in structural analysis and design.
A generalised step-by-step procedure for fatigue crack growth analysis of structural components subjected to variable amplitude loading spectra has been presented.
Fractured surfaces were inspected and fatigue data were analyzed using a standard procedure for calculation of fatigue life with a semi-elliptical surface crack assumption was performed; from which parameters of the Paris law for fatigue fracture were obtained.
The required elements and the procedure for fatigue failure analysis and life estimation of a welded structure are explained.
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