2021
DOI: 10.17559/tv-20200414015501
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Initial Fatigue Life Estimation of Welded Structural Components

Abstract: Numerical modelling of welding process of two cylindrical tubes subjected to cyclic loads of constant amplitude is presented. For that purpose the Finite Element Method (FEM) was used for determination of thermo-mechanical behaviour and evaluation of welded joint residual stresses. In this investigation an efficient computation method for initial fatigue life estimation of welded structural components has been developed. Computation method with corresponding computation procedure is based on finite element num… Show more

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Cited by 5 publications
(5 citation statements)
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“…For structural analysis of sandwich and thin-walled composite wing Finite Element Method (FEM) was used [9, 11-14, 19, 25, 26]. These results, later on, are compared with the own experimental test results [10,15,23,27,28]. After the numerical stress analysis of the UAV composite structure, usually, experimental tests are undertaken.…”
Section: Experimental Static Testing and Comparison With Numerical Resultsmentioning
confidence: 99%
“…For structural analysis of sandwich and thin-walled composite wing Finite Element Method (FEM) was used [9, 11-14, 19, 25, 26]. These results, later on, are compared with the own experimental test results [10,15,23,27,28]. After the numerical stress analysis of the UAV composite structure, usually, experimental tests are undertaken.…”
Section: Experimental Static Testing and Comparison With Numerical Resultsmentioning
confidence: 99%
“…Also, in the previous ten years, there has been a significant increase in the production of energy from RES in the world, primarily energy from wind [1,29,36] and solar [29] while in Serbia, these two energy sources are still at modest levels. In this regard, the RES strategy in the coming period should go in two directions.…”
Section: Discussionmentioning
confidence: 99%
“…Nowadays, most engineering tasks using numerical analysis are solved with satisfactory results using linear numerical approximation, that is, by applying the basic equation of the finite element method [11][12][13][14][15][16][17][18]. Given that nonlinear problems are more complex and cannot be described by the basic equation of the finite element method, it is necessary to define a nonlinear relation that is given by the expression [11]:…”
Section: Finite Element Analysis Of the Shrink Fitmentioning
confidence: 99%
“…Figure18 Dependence of the maximum value of the contact pressure on the rotor speed for the mean interference value[11] …”
mentioning
confidence: 99%