TRANSMISSION AND REFLECTION OF AO MODE LAMB WAVE IN A PLATE OVERLAP Won-Joon Song1, Joseph L. Rose1, Jose M. Galan2, and Ramon Abascal2 Ultrasonic Lab, Department of Engineering Science and Mechanics, Penn State University, University Park, PA 16802, USA 2 Escuela Superior de Ingenieros Camino de los Descubrimientos, s/n. E41092, Sevilla, Spain ABSTRACT. Lamb wave propagation in a plate overlap is investigated. Transmission and reflection coefficients for incident Lamb waves of AO mode across the overlap region are numerically calculated using a hybrid BE-FE method. Transmission and reflection coefficients of the Lamb wave across the overlap region are studied as a function of frequency and overlap length. In addition, mode conversion phenomena from the incident waves within the overlap region are also included in the numerical study. A few experiments were also conducted for measurements of transmission and reflection coefficients for incident AO mode wave in overlap-shaped steel plates with two different overlap areas. The experimental results are in good agreement with the numerical calculations. The numerical and experimental results can be used to establish guidelines for NDE in overlapped plates and in multilayer structures with various joints by selecting modes and tuning frequency. INTRODUCTION Ultrasonic guided wave techniques using have been successfully applied to plate-like structures, pipes, rods, and multilayer structures due to the characteristics of guided waves such as long propagation distances, controllability of sensitivity to defects, and high penetration power [1, 2, 3]. The geometry of industrial structures becomes more complex than simple structures like pipes, rods, etc. In order to evaluate these complex structures, ultrasonic waves should be able to travel through branch, weld, and overlap joints. In many cases, this geometrical complexity in the structure causes difficulties in their effective nondestructive evaluation because of scattering and the existence of hidden areas. It has been reported that applications of guided wave NDE already extend to such structures with complex geometry as lap-jointed plates, rails, curved pipes, rods with an arbitrary cross-section and overlapped plates [4 -8]. CP657, Review of Quantitative Nondestructive Evaluation Vol. 22, ed. by D. O. Thompson and D. E. Chimenti © 2003 American Institute of Physics 0-7354-0117-9/03/$20.00 1088 In this study, guided wave scattering in a plate with an overlap is numerically and experimentally studied in terms of frequency and overlap dimensions. The overlap region simulates a perfect joint of two semi-infinite plates. A Hybrid Boundary Element (BE)Finite Element (FE) technique is employed to numerically calculate the scattering of guided waves from an overlap, which combines a Boundary Element method with a semi-analytical Finite Element method and a normal mode expansion [9 - 14]. Mode conversion within the overlap region is also considered in the numerical calculation. The transmission and reflection of AO Lamb wave impinging on an overlap are experimentally measured for comparison with the numerical results. NUMERICAL CALCULATION OF TRANSMISSION AND REFLECTION FACTORS FOR AO MODE INCIDENT LAMB WAVE. A hybrid Boundary Element (BE)- Finite Element (FE) method was utilized in order to calculate the transmission and reflection factors in a plate overlap. In this hybrid BE FE technique, the guided wave scattering problem is solved by defining two regions as shown in Figure 1. The neighborhood of the defects is discretized with a quadratic Boundary Element method and the elastodynamic solution in each waveguide is expressed as a normal mode expansion [9, 12, and 13]. Each semi-infinite plate region is modeled with a FE technique based on a semi-analytical formulation of the wave propagation in a plate, from which an absorbing boundary condition is derived that will be later applied on the BE region [14]. The FE and BE regions are coupled by equilibrium and compatibility on their common interface. The transmission and reflection factors are numerically calculated as mode conversion factors. In this paper, they are defined as __ where C)m) is the mode conversion factor for the scattered mode m under the incidence of mode /, E(m) is the energy flux averaged over a period carried by the propagating mode Boundary Element Method in overlap region pinite Element Method in semi-infinite plate region • • • • • • • • • • • • • • • • i Finite Element Method in semi-infinite plate region Transmitted wave Incident wave Reflected wave Absorbing boundary condition FIGURE 1. Illustration of the boundary configuration for a hybrid Boundary Element-Finite Element method in a plate overlap. 1089 m through any cross section of the plate, Einc is the total incident energy, and a(m} is the participation coefficient of mode m in the normal mode expansion of the scattered field. By a normalization procedure which SQtsE(m} equal to unity for all modes m, the mode conversion factors between the incident and the scattered modes are equal to the participation coefficients. The numerical results include the factors for mode converted waves (secondary mode conversion factors) as well as for the same mode as the incident mode (primary mode conversion factors). Transmission and reflection factors over an overlap region are calculated as a function of frequency for AO mode incident Lamb wave. The material properties used in the numerical study are those of steel: CL = 5.9 mm/jusec, CT= 3.2 mm/fisec, and density 7.8 g/cm3. The problem geometry corresponds to two 6.35 mm thick plates with a 12.7 mm thick overlap region. First, a case with a fixed overlap length of 6.35mm is considered. The higher modes generated by mode conversion phenomena within the overlap region beyond their first cut-off frequency up to 1.5 MHz are also calculated. The calculation results show that the transmission and reflection factors across the overlap region vary dramatically along frequency as shown in Figures 2. The peaks or valleys of these transmission and reflection factors are obtained in narrow frequency ranges. In the frequency range beyond the first cut-off frequency, a significant amount of energy is transferred from the incident mode into the higher converted modes in the scattered field. Furthermore, a parametric study over the overlap length is performed with the overlap parameter ranging from 0.5 to 13mm. Figure 3 presents the contour map plots of the primary transmission and reflection factors for AO Lamb mode as a function of frequency and overlap length. It is noted that the transmission and reflection of AO Lamb wave in a plate overlap is a complicated phenomena with respect to frequency and overlap length. In general, a high level of transmission (low in reflection) over the plate overlap occurs in the frequency range lower than 100 kHz for all the overlap lengths. But, maxima in the primary mode conversion factors are localized in the frequency-overlap length plane as shown in Figure 4. MEASUREMENTS ON TRANSMISSION AND REFLECTION FACTORS OF AO MODE LAMB WAVE Experimental Setup Experiments were conducted in two steel plates with an overlap. A 12.7 mm thick steel plate was machined into the half-thickness overlapped plates leaving a 12.7 mm thick overlap region and 6.35 mm thick transmitting and receiving regions. The overlap lengths, L, are 6.35 and 12.7 mm (Plates 1 and 2 respectively). Two variable angle transducers are located with a total wave path of 304.8 mm in both through-transmission and pulse-echo configurations. For reflection factor measurement, the transducers are located at an angle of 15 degrees with respect to the central line in order to avoid the beam divergence effect in the transducers. The incident wedge angles of the transmitter and receiver are identical so that the same scattered mode as the incident mode is collected (primary conversion factor). The peak-to-peak amplitude of scattered waves were measured and transmission and reflection factors were calculated as the ratio of the 1090 1 1 A0 A1 A2 A3 A4 0.8 A0 A1 A2 A3 A4 0.8 0.6 0.6 T R 0.4 0.4 0.2 0.2 0 0 0 0 .5 0.5 11 (M H z) FF rree qq uu ee nn ccyy (MHz) 0 1.5 1.5 1 S0 S1 S2 S3 S4 0.8 1.5 1.5 (b) (a) 1 0 .5 0.5 11 (M H z) FFrre e qquueennccyy (MHz) S0 S1 S2 S3 S4 0.8 0.6 0.6 T R 0.4 0.4 0.2 0.2 0 0 0 0 .5 0.5 11 F rree qq uu ee nn cc yy (MHz) (M H z) F 1.5 0 0 .5 0.5 11 (M H z) FFrre e qquueennccyy (MHz) 1.5 1.5 (d) (d) (c) (C) FIGURE of the the transmission transmission and and reflection reflection factors factors for forAO A0incident incidentmode modeininaa6.35 6.35 FIGURE 2. 2. Numerical Numerical calculation calculation of mm plate with with aa 6.35mm 6.35mm long long and and 12.7 mm thick thick overlap overlap region, region. (a) (a) Reflection Reflection factor factor for for mm thick thick steel steel plate 12.7 mm antisymmetric Transmission factor factor for for antisymmetric antisymmetric modes, modes, (c) (c) Reflection Reflection factor factor for for antisymmetric modes, modes, (b) (b) Transmission symmetric factors for for symmetric symmetric modes. modes. symmetric modes, modes, and and (d) (d) Transmission Transmission factors amplitude waves to to that that of of the the reference reference waves waves which which were were amplitude of of the the transmitted transmitted or or reflected reflected waves collected thick plain plain steel steel plate. plate. collected in in aa 6.35mm 6.35mm thick Experimental Experimental Results Results Figure 4 shows the measured transmission transmission and and reflection reflection factors factors of of AO A0 Lamb Lambmode modeinin comparison with numerical results. In general, the comparison the overall overall experimental experimentalmeasurements measurementsare are in good good agreement with numerical calculations. The in The experimental experimental results results indicate indicate that thatthe the transmission and reflection of Lamb waves impinging transmission impinging on on an an overlap overlap region region can can be be maximized or minimized for each incident maximized incident mode mode in in aa specific specific frequency frequency range range asas predicted in numerical calculations. The maximum predicted maximum transmission transmission occurs occurs at at 250 250 kHz kHz and and 530 ~~ 550 550 kHz for 6.35 mm long overlap and at 530 at 185 and and 500 500 kHz kHz for for 12.7 12.7 mm mm long long overlap, while the maximum reflection overlap, reflection occurs at 200 200 kHz kHz for for 6.35 6.35mm mmlong longoverlap overlapand and at 150, 150, 250 , and 410 kHz for 12.7 at 12.7 mm mm long long overlap. overlap. These experimental results demonstrate the possibility These possibility of of controlling controlling the the Lamb Lamb wave wave transmission and reflection from an overlap region by transmission by selecting selecting proper proper incident incident mode mode and and frequency. In view of practical application, these results frequency. results can can provide provide aauseful usefulguideline guidelinetoto 1091 • 0.9-1 fflO.8-0.9 £30.7-0.8 a 0.6-0.7 a 0.5-0.6 C3O.4-O.5 d 0.3-0.4 EDO.2-O.3 CUO.1-O.2 0.0 0.2 0.3 0.5 0.6 O.S O.9 1 .1 1 .2 na-o.1 1 .4 (a) 13 0.9-1 0.8-0.9 10.5 El 0.7-0.8 a 0.6-0.7 3 D 0.5-0.6 5.5 OO.4-Q.5 a 0.3-0.4 3 nO.2-O.3 a 0.1-0.2 no-a.1 0.5 O.O O.2 0.3 O.S O.6 O.S O.9 1 .1 1 .2 1 .4 Frequency. MHz (b) (b) FIGURE3.3.Numerical Numericalcalculation calculationof ofprimary primarymode mode conversion conversion factors factors for forAO A0Lamb Lamb mode mode as as aa function function of of FIGURE frequencyand andoverlap overlaplength, length.(a) (a)Transmission Transmissionfactor, factor,(b) (b)Reflection Reflectionfactor. factor. frequency 1 .0 1 .0 Ex p Nu m 0 .8 Ex p Nu m 0 .8 0 .6 0 .6 R T 0 .4 0 .4 0 .2 0 .2 0 .0 0 .0 0 0 .2 0.2 0 .4 0 .6 Fr e q u e0.4 n c y ( M Hz ) 0.6 F r e q u e n c y (MHz) 1 .0 0 .8 0 0 .4 Fr e q u e 0.4 n c y ( MHz ) 0 .6 0.6 1 .0 Ex p Nu m 0 .8 0 .6 0 .8 F r e q u e n c y (MHz) (a) fa) Ex p Nu m 0 .8 0 .2 0.2 0 .6 T R 0 .4 0 .4 0 .2 0 .2 0 .0 0 .0 0 0 .2 0.2 0 .4 0 .6 Fr e q u e0.4 n c y ( M Hz ) O.I 0 .8 0 F r e q u e n c y (MHz) 0 .2 0.2 0 .4 0 .6 Fr e q u e0.4 n c y ( M Hz ) 0.6 F r e q u e n c y (MHz) 0 .8 (b) (b) FIGURE 4. Comparison of experimental measurements with numerical calculation on transmission and FIGURE 4. Comparison of experimental measurements with numerical calculation on transmission and reflection factors for A0 Lamb incident mode. (a) Transmission and reflection factors with the overlap reflection factors for AO Lamb incident mode, (a) Transmission and reflection factors with the overlap length of 6.35 mm, (b) Transmission and reflection factors in the overlap length of 12.7 mm. length of 6.35 mm, (b) Transmission and reflection factors in the overlap length of 12.7 mm. 1092 effective guided wave NDE in the area of a plate before or beyond the overlap region and inside the overlap region itself. CONCLUSIONS The scattering of guided waves in a plate overlap has been studied numerically and experimentally. The numerical studies are performed using a hybrid BE-FE technique. First, a plate overlap of fixed geometry is considered, for which the primary and secondary mode conversion factors under AO Lamb incidence are calculated. It is found that the scattering of Lamb waves by the overlap region has a complicated pattern along the frequency. High values of transmission and reflection factors are obtained within narrow frequency ranges. The mode conversion phenomena from the overlap region above the first cut-off frequency produces higher modes in the scattered field, and the interference among the modes results in a complicated scattering pattern along the frequency. Next, a parametric study is performed for varying geometries, which reveals that the primary mode conversion factors highly depend on the incident wave mode, overlap dimensions and frequency. The maximum transmission and reflection for each incident mode are obtained within localized frequency-overlap length ranges. The experiments on measurement of transmission and reflection factors for AO Lamb wave agree well with the numerical calculation. Therefore, it can be concluded that best reflection and transmission points can be obtained by tuning phase velocity and frequency and observing maximum amplitude signals to find its best test points. In addition, the numerical studies can provide quantitative prediction of Lamb wave scattering over an overlap. REFERENCES 1. Rose, J.L., "Ultrasonic Waves in Solid Media", Cambridge University Press, Cambridge, (1999). 2. Rose, J.L., "Guided wave nuances for ultrasonic nondestructive evaluation", IEEE Transaction on Ultrasonics, Ferroelectrics, and Frequency Control, 47, 575-583 3. 4. 5. 6. 7. (2000). Achenbach, J.D., "Wave Propagation in Elastic Solid", North-Holland, New York, (1973). Lowe, M.J.S., Challis, RE., and Chan, C.W., "The transmission of Lamb waves across adhesively bonded lap joints", Journal of Acoustical Society of America, 107, 1333-1345 (2000). 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