1976
DOI: 10.1016/0029-1021(76)90240-1
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Crack depth measurement in rail steel by Rayleigh waves aided by photoelastic visualization

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Cited by 25 publications
(5 citation statements)
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“…For reflection from edges and grooves see also [1186,1187,1606,1607,50,229,544,394], for picture displays see [597], for computer simulations see Sato [1321] and Harumi [617, 9, 618, 619, S 65]. Angles other than 90 0 are less interesting, but if the angle of incidence of a longitudinal wave (Fig.…”
Section: Reflection At a Right-angled Edge And In A Comermentioning
confidence: 97%
“…For reflection from edges and grooves see also [1186,1187,1606,1607,50,229,544,394], for picture displays see [597], for computer simulations see Sato [1321] and Harumi [617, 9, 618, 619, S 65]. Angles other than 90 0 are less interesting, but if the angle of incidence of a longitudinal wave (Fig.…”
Section: Reflection At a Right-angled Edge And In A Comermentioning
confidence: 97%
“…In 1967, Viktorov proposed measuring the change in period of oscillation in the frequency domain to determine the defect depth [16]. This approach was enhanced further by Domarkas et al and Hall et al, whose research facilitated the determination of defect length via pulse time measurement [17,18]. In the research conducted by Papaelias et al, it was concluded that defect detection is optimised when transmitting ultrasound waves at incident angles of 0 • , 37 • , 45 • and 70 • [19].…”
Section: State Of the Artmentioning
confidence: 99%
“…Once the wave encounters the crack, interaction with the latter occurs. There exists a vast literature (for example [105,106,107]) about the interaction phenomena between Rayleigh waves and cracks in solids. Part of the wave is transmitted through the crack location; part is reflected back in opposite direction (clearly visible in Figure 4.100d-f); part propagates along the edges of the crack (visible in Figure 4.99c); finally, mode conversions will occur, and bulk waves are generated from the tips of the crack which act as secondary sources (visible in Figure 4.99c and Figure 4.100d).…”
Section: Air Modelingmentioning
confidence: 99%