2015
DOI: 10.1016/j.ymssp.2015.01.021
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Non-linearities in the vibrations of elastic structures with a closing crack: A state of the art review

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Cited by 157 publications
(81 citation statements)
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“…The second case study concerns the spar of a prototype wing, the linear and nonlinear dynamics of which have been investigated in recent studies [62,63]. Importantly, the prototype skin is supposed to completely transfer the aerodynamic loads to the spar, making the structural behaviour of the latter a good approximation of the dynamical response of the whole spar-skin ensemble.…”
Section: High Aspect Ratio Flexible Wingmentioning
confidence: 99%
“…The second case study concerns the spar of a prototype wing, the linear and nonlinear dynamics of which have been investigated in recent studies [62,63]. Importantly, the prototype skin is supposed to completely transfer the aerodynamic loads to the spar, making the structural behaviour of the latter a good approximation of the dynamical response of the whole spar-skin ensemble.…”
Section: High Aspect Ratio Flexible Wingmentioning
confidence: 99%
“…The relationship between crack parameters and 2× amplitudes at 1/3 critical speed can be written as: Y = f(l, d) = f(x), where, l and d are vectors for crack locations and crack depths respectively and x is the crack parameters set. Specifically, the relationships for measurement points A and B are Y 1…”
Section: Construction Of the Crack Kriging Surrogate Modelmentioning
confidence: 99%
“…Because of these, a cracked rotor possesses complex dynamic characteristics. Much work on the dynamic behavior of cracked rotors has been performed to identify cracks in rotors, and a number of reviews on this topic [1][2][3][4][5][6][7] have been published. From the literature, vibration-based crack identification methods can be broadly classified as model-based Based on the above short review, there is a trend to transform the crack identification problem into an optimization problem, and through updating iterations to find the crack parameters minimizing the difference between measured features and calculated features, which can be classified as model updating method [36].…”
Section: Introductionmentioning
confidence: 99%
“…So, crack monitoring for rotors is very important, which includes four levels: crack detection, crack localization, crack severity assessment and remaining service life prediction. Many studies have been carried out based on vibration signature in the past few decades, which has been well documented in the review papers . However, most research focus on crack detection, that is, to determine if any cracks exist in a rotor.…”
Section: Introductionmentioning
confidence: 99%