2020
DOI: 10.3390/s20236847
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A Machine Learning Approach to Model Interdependencies between Dynamic Response and Crack Propagation

Abstract: Accurate damage detection in engineering structures is a critical part of structural health monitoring. A variety of non-destructive inspection methods has been employed to detect the presence and severity of the damage. In this research, machine learning (ML) algorithms are used to assess the dynamic response of the system. It can predict the damage severity, damage location, and fundamental behaviour of the system. Fatigue damage data of aluminium and ABS under coupled mechanical loads at different temperatu… Show more

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Cited by 16 publications
(18 citation statements)
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References 39 publications
(46 reference statements)
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“…These dynamic responses contain information regarding the locations and sizes of the crack(s). Many researchers have focused on the vibration characteristics of cracked beams [ 1 , 7 , 8 , 9 , 10 , 11 , 12 , 13 , 14 , 15 , 16 , 17 , 18 , 19 , 20 , 21 , 22 , 23 , 24 , 25 , 26 , 27 , 28 , 29 , 30 , 31 , 32 , 33 , 34 , 35 , 36 , 37 , 38 , 39 , 40 , 41 , 42 , 43 , 44 , 45 ]. Ostachowicz and Krawczuk (1991) modelled the crack as a torsional spring model and calculated the natural frequencies of single-sided and double-sided crack cantilever beams [ 46 ].…”
Section: Introductionmentioning
confidence: 99%
“…These dynamic responses contain information regarding the locations and sizes of the crack(s). Many researchers have focused on the vibration characteristics of cracked beams [ 1 , 7 , 8 , 9 , 10 , 11 , 12 , 13 , 14 , 15 , 16 , 17 , 18 , 19 , 20 , 21 , 22 , 23 , 24 , 25 , 26 , 27 , 28 , 29 , 30 , 31 , 32 , 33 , 34 , 35 , 36 , 37 , 38 , 39 , 40 , 41 , 42 , 43 , 44 , 45 ]. Ostachowicz and Krawczuk (1991) modelled the crack as a torsional spring model and calculated the natural frequencies of single-sided and double-sided crack cantilever beams [ 46 ].…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, the stress amplitude σ i (l c ) was used to show the stress range per cycle instead of the difference among the peak and trough as shown in Equation (12). After that, the bending moment 𝑀 (𝑙 ) at the crack location in i th cycle can be calculated by Equation (10):…”
Section: Calculation Of Sif Range and Fcg Ratementioning
confidence: 99%
“…These structures can experience fatigue failure due to dynamic loads in a complex thermo-mechanical environment [10][11][12]. Compared with other materials [13][14][15][16][17], the crack propagation during fatigue is highly complicated for FDM polymeric structures because of the significant differences in its microstructure due to various printing parameters.…”
Section: Introductionmentioning
confidence: 99%
“…In the literature, the vibration or dynamic response of cracked structures has been investigated by different approaches [2,[22][23][24][25][26][27][28][29][30][31][32][33][34][35]. However, the existing research on crack growth did not consider the effect of the rate of heating with different temperature exposure times.…”
Section: Introductionmentioning
confidence: 99%