2018
DOI: 10.1016/j.ijfatigue.2018.05.014
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Nonlinear ultrasonic modulation based failure warning for aluminum plates subject to fatigue loading

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Cited by 40 publications
(17 citation statements)
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“…The nonlinear parameter is inversely proportional to the excitation amplitudes and wavenumbers of two incident waves as shown in Equations ( 1 ) and ( 2 ): and where and are modulated material nonlinear parameters; and are wavenumbers of two incident waves; and and are amplitudes of two incident waves, respectively [ 39 , 40 ]. The nonlinear parameters and are constants corresponding to sideband frequencies (HF-LF) and (HF+LF), respectively.…”
Section: Quantitative Analysis Of Wave Modulation With Seam Crackmentioning
confidence: 99%
“…The nonlinear parameter is inversely proportional to the excitation amplitudes and wavenumbers of two incident waves as shown in Equations ( 1 ) and ( 2 ): and where and are modulated material nonlinear parameters; and are wavenumbers of two incident waves; and and are amplitudes of two incident waves, respectively [ 39 , 40 ]. The nonlinear parameters and are constants corresponding to sideband frequencies (HF-LF) and (HF+LF), respectively.…”
Section: Quantitative Analysis Of Wave Modulation With Seam Crackmentioning
confidence: 99%
“…In this study, the first modulation components (A + M and A À M ) are used for prognosis because (1) the modulation components are less affected by other sources of nonlinearities induced by transducers or data acquisition (DAQ) systems, and (2) selecting the frequencies and modes of input ultrasonic signals is more flexible compared with the use of a harmonic technique. 26,27 In general, the nonlinearity produced by a fatigue crack is represented using the nonlinear parameter (b parameter) obtained by normalizing the amplitudes of modulation components with respect to the amplitudes of input signals as follows [19][20]24 b =…”
Section: Nonlinear Parameter For Fatigue Crack Assessmentmentioning
confidence: 99%
“…Similar trends are also observed in experiments on additional aluminum plate specimens with different thicknesses. 19 The growth of a fatigue crack can be described using the Paris-Erdogan equation, and it is written as…”
Section: Nonlinear Parameter For Fatigue Crack Assessmentmentioning
confidence: 99%
“…SHM is a revolutionary innovation technology to determine the structural integrity and a key technology to improve the operation safety of advanced equipment, and moreover can improve the present design concept of damage tolerance [ 4 ]. There are some SHM technologies which have been used for the damage monitoring of bolted joints, such as ultrasonic guided wave [ 5 , 6 , 7 ], electromechanical impedance [ 8 , 9 ], comparative vacuum monitoring sensor [ 10 ], vibration [ 11 ], acoustic emission [ 12 ] and so on. However, these technologies have the following problems: (1) It is difficult to identify the cracks in the non-surface layer of a multi-layer jointed structure; (2) It is difficult to accurately quantify the angle of hole edge cracks, and then identify the failure mode.…”
Section: Introductionmentioning
confidence: 99%