2019
DOI: 10.1016/j.ymssp.2018.11.016
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Pulsed laser-scanning laser Doppler vibrometer (PL-SLDV) phased arrays for damage detection in aluminum plates

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Cited by 54 publications
(24 citation statements)
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“…The side length of the damage is 10 mm, and the depth is 0.5 mm (Figure 2(a)). A 3-count toneburst at 120 kHz is used where we can achieve dominant A 0 mode that has strong out-of-plane motion for SLDV sensing (Tian et al, 2019). The wavelength is about 8.7 mm, which is appropriate for the intended damage detection conducted in this study (Alleyne and Cawley, 1992; Cawley, 1997).…”
Section: Detection and Resultsmentioning
confidence: 99%
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“…The side length of the damage is 10 mm, and the depth is 0.5 mm (Figure 2(a)). A 3-count toneburst at 120 kHz is used where we can achieve dominant A 0 mode that has strong out-of-plane motion for SLDV sensing (Tian et al, 2019). The wavelength is about 8.7 mm, which is appropriate for the intended damage detection conducted in this study (Alleyne and Cawley, 1992; Cawley, 1997).…”
Section: Detection and Resultsmentioning
confidence: 99%
“…Recently the scanning laser Doppler vibrometer (SLDV) attracts great interests for Lamb wave wavefield data based damage detection, quantification, and SHM/NDE (Harb and Yuan, 2016; Rogge and Leckey, 2013; Staszewski et al, 2004; Tian et al, 2019; Yu et al, 2013, 2015). The SLDV works on the Doppler effect and can measure the Lamb wave particle motion in terms of velocities or displacement along the laser beam.…”
Section: Introductionmentioning
confidence: 99%
“…The specific guided-wave parameters and the energy skew effects are also taken into account for anisotropic materials [20]. The use of receiver bemforming and laser Doppler vibrometer have been further explored in damage detection and quantification in composite structures [21], and in an improved damage identification approach in aluminum plates by a modified DAS algorithm [22].…”
Section: Background Of Beamforming Techniquesmentioning
confidence: 99%
“…Lamb wave-based structural health monitoring (SHM) technique has been proved to be one of the strongest techniques for online and real-time damage detection of aircraft structures because of the superior capability of travelling long distances and covering large monitoring area with limited numbers of piezoelectric sensors [1]. Plenty of Lamb wave-based damage detection algorithms, including delay and sum [2,3], phased array [4,5], tomography [6,7,8,9,10,11], and migration [12,13], have been developed. Comprehensive reviews on the application of Lamb wave for structural health monitoring can be found in the literature [1,14,15].…”
Section: Introductionmentioning
confidence: 99%
“…Comprehensive reviews on the application of Lamb wave for structural health monitoring can be found in the literature [1,14,15]. Depending on whether reference data of Lamb wave in the pristine structure is needed or not, these algorithms can be divided into two categories, i.e., reference-free algorithms [16,17,18,19] and reference-dependent ones [2,3,4,5,6,7,8,9,10,11,12,13]. Reference-dependent algorithms are more practical than reference-free ones for real application in aircraft structures due to the complex nature of the Lamb wave, including multiple mode, modes conversion and scattering at the boundary.…”
Section: Introductionmentioning
confidence: 99%