Shearographic detection of delaminations in sandwich structures: investigation on various excitation modes G.Kalogiannakis1,2, B. Sarens2, D. Van Hemelrijck1 and C. Glorieux2 1 Dept of Mechanics of Materials and Constructions, Vrije Universiteit Brussel, Belgium 2 Laboratory of Acoustics and Thermal Physics, Dept of Physics and Astronomy, Katholieke Universiteit Leuven, Belgium ABSTRACT Sandwich structures are increasingly used in engineering constructions wherever the design specifications demand the combination of light structures with high bending stiffness. The most common defects of such structures are the so-called delaminations, which occur between the core and the skins and originate from existing manufacturing flaws or the loading conditions. This study was focused on the detection of such defects with digital shearography in a dynamic mode compared to competitive nondestructive testing (NDT) techniques. The material under investigation was Polymethacrylamide rigid foam used as core reinforced with woven as well as unidirectional (UD) Carbon/Epoxy layers. Introduction Sandwich materials are light weight structures, which are especially oriented to satisfy design requirements for high bending stiffness. To this end, the core, a typically rather thick material of low density and strength, is combined with thin (and therefore low bending stiffness) skins of high tensile strength [1]. It is evident that a critical factor for the performance of the sandwich structure is the quality of the adhesion between the skins and the core. Manufacturing flaws and/or compressive or impact loads, which may increase dramatically the interlaminar shear stresses, may often initiate and result in the local debonding of the layers. Such defects are very common in sandwich structures and they are so-called delaminations. The timely detection becomes critical for the evaluation of the residual strength of the structural component as this defect may lead to local or global buckling and eventually failure of the structure [2-5]. Consequently, various NDT methods are dedicated to the detection and characterization of delaminations. The methods are generally divided in full-field and scanning depending on whether we can obtain directly (in a single step) the image of the object under investigation or we have to scan in a raster-like manner over the surface. It is reasonable that, in the recent years, the full-field techniques gain increasingly ground due to their efficiency and operation speed, especially for large structures. Full-field techniques are basically transient [6-7], lock-in [8] and ultrasound lock-in thermography [9-10], as well as the speckle pattern interferometric techniques [11-13]. In principle, the thermographic techniques make use of an IR camera to detect the perturbations in the temperature field due to the disruption in the heat flow by the embedded delaminations while the object is thermally excited. In the first two cases, the heat is generated through the surface by means of a laser or halogen lamps and in the case of ultrasound lock-in thermography the heat is generated locally around the defects due to hysteresis and friction by means of an ultrasonic welder or a shaker. In contrast, speckle techniques, namely electronic speckle pattern interferometry (ESPI) and shearography make use of a normal charge-coupled device (CCD camera) to record an image of the object before and after loading. They are based on the speckle effect, which is a light interference phenomenon occurring when coherent light like a divergent laser beam is diffusely scattered on an optically rough surface (roughness of the order of the optical wavelength). In classical interferometry, a laser beam is passing through a beam splitter and one part is reflected on a fixed reference plate, while the other is reflected on the object under investigation and the two beams are superposed on an optical detector. When the object is displaced along the direction of the optical path, the phase difference between the two laser beams is accordingly changed resulting in a change of the light intensity on the detector. In speckle techniques, the so-called objective speckles are formations of random optical interference in space from light rays coming from different places on the object, and their size and intensity change with the distance from the object. Such a speckled image pattern of the object under investigation is recorded using a camera with each individual pixel acting as a separate optical detector, which probes the displacement of a respective area on the object. Adjusting the aperture and the distance of the lens from the object controls the size of the recorded so-called subjective speckle and therefore the size of the respective area on the sample. Subtraction of successive images before and after loading results in a fringe pattern which is directly associated to the change of the optical path and therefore the absolute displacement of the object under investigation. The interferometric setup of shearography in particular consists of a rotating mirror. As a result the recorded image is the superposition of two images slightly sheared with one another. Each pixel represents thus the relative position of two points (slope) on the object before and after loading. Therefore, shearography is suited to measure deformations and strains rather than absolute displacements. The advantage is that the technique has no need for a reference beam and the sensitivity to rigid body motions is considerably suppressed. This is why the method is widely appreciated and well established in the industry. The process of the evaluation of the fringe pattern (interferogram), although usually not required, is depicted in Figure 1. In order to determine the absolute or relative phase difference of the different gray intensity levels, one has to apply the so-called phase stepping. By applying successive changes of the optical path of the probing beam, one can evaluate the dependence of the intensity on the relative phase. The resulting phase image has to be filtered and normalized before the demodulation process where by taking a reference the phase is unwrapped. The result is integrated to give the deformation in one or two directions. Figure 1. The quantification process of the speckled fringe pattern. In what follows, we shall demonstrate how the method was used in a dynamic mode in order to detect artificial delaminations in composite sandwich structures and present the advantages as well as the disadvantages with respect to the competitive lock-in thermography. Material Sandwich plates were manufactured using woven (Hexply 920CX-793-50%) as well as unidirectional (Hexcel - Fibredux 920CX-TS-5-42) Carbon/Epoxy prepregs for the skins and polymethacrylimide (PMI – Rohacell 71) as core. This type of material was selected as it is typically used in advanced applications where any material failure is critical for the safety of human lives. Regarding the manufacturing process, a lot of effort has been put recently in order to optimize the curing procedure [14] based on the thermal and mechanical properties and their variance. (a) (b) Figure 1. Specimens with embedded defects –dimensions are given in mm-.(a) sandwich plate (plate A) with circular delaminations of different diameters, and (b) a plate with square defects of different materials (plate B). Artificial delaminations of different geometries were created in the plates by placing thin Teflon films (thickness of 10μm) between the core and the skins in order to evaluate the possibility to characterize the defects. Other types of defects like inclusion of Al or St foils (thickness of 15μm) were also induced so as to compare the probability of detection for the different methods under consideration. Since the plates undergo the curing procedure under high temperature and uniform pressure the resulting surface is smooth and there is no externally visible indication of the delaminations. The exact dimensions of the plates and the embedded defects under investigation are shown in Figure 1. The plate on the left had a single woven layer while the one on the right had two UD layers symmetrically placed on either side. Experiments Experiments were carried out using two different setups related to shearography and lock-in thermography. The former setup is depicted in Figure 2. In principle, for the implementation of stroboscopic shearography, the object under investigation is illuminated at particular instances with a successive increment of the phase difference with respect to the initial point of the excitation. By evaluating the deformation at each step with respect to the reference, one can thereby reconstruct the full harmonic motion of the vibrating object. The setup also provides the flexibility for comparison with a scanning laser Doppler vibrometer. It also allows for the simultaneous excitation with a shaker (Brüel & Kjær) and a piezoelectric transducer so as to investigate nonclassical acoustic nonlinearities. Figure 2. Shearography Figure 3. Lock-in thermography The setup which was used for the experiments of lock-in thermography is shown in Figure 3. A powerful (30W) diode laser (λ=810nm – Coherent FAP I) is electro-optically modulated by means of an electrical signal that we provide through a data acquisition card (DAQ NI PCI 6024E). The same signal is used as a reference for the lock-in procedure of the infrared images which are recorded. In the alternative approach of ultrasound lock-in thermography the same signal can be used to modulate the high frequency wave of an ultrasonic transducer. Results The composite sandwich plates were examined dynamically with shearography in a stroboscopic mode. Linear as well as nonlinear approaches were used in order to evaluate the detectability of the defects, analyze the differences and compare the results. In Figure 4, the results are shown for the excitation of plate A by means of the piezoelectric transducer at 10, 20 and 50kHz. The image is zoomed around the delamination of 28mm, with the circle indicating the underlying delamination. The feature on the right hand side of the lower part is the piezoelectric transducer. To visualize defects in the linear regime, one has to excite the object under investigation at one of the resonance frequencies of the thin upper layer lying over the delamination. In Figure 4, it is apparent that for 10kHz the delamination is hardly visible while for 20 and 50kHz we obtain the two first mode shapes which clearly indicate the position of the delamination. (a) (b) (c) Figure 4. Fringe patterns of the sandwich plate obtained with shearography. Excitation is carried out with a piezoelectric transducer at (a)10, (b)20 and (c)50kHz. A recent advancement [15] in shearographic visualization of defects is depicted in Figure 5. The so-called cross-modulation effect due to the contact acoustic nonlinearity [16-20] is visualized in a single shot. The plate A was excited simultaneously by the piezoelectric transducer as well as a shaker at 50 and 5 kHz respectively. The image is zoomed around to the delaminations with diameters of 34 and 28mm. In principle, a strong low frequency wave acts as a pump opening and closing the defect. It becomes thus a carrier for the high frequency wave, which is amplitude modulated. This is an effect which occurs in such a case only above the defects and is a so-called nonclassical acoustic nonlinearity. The piezoelectric transducer has the double size of the one related to Figure 4 (diameter of 4cm) and is located at the upper right hand side. In the figure we observe that at 50kHz the defects are hardly visible while at 5kHz the defects have a certain influence on the distortion of the fringe pattern giving an indication about the location of the delaminations. When we apply both excitations at the same time and look at the images obtained for the sum or the difference of the frequencies, the resulting patterns correspond directly to the underlying defects. What is clearly apparent from the image of the difference is that the adhesion of the skin and the core between the two artificial delaminations is inadequate. This claim was examined and confirmed with the laser Doppler vibrometer. (a) (b) (c) Figure 5. Fringe patterns of the sandwich plate obtained while it is excited simultaneously by a shaker and the piezoelectric transducer at 5kHz and at 50kHz respectively. (a)image obtained with only 50kHz excitation, (b) image obtained with only 5kHz excitation and (c) image obtained with both excitations active and shearography locked at their difference. A similar result with two frequencies which are closer to one another, 20 and 25kHz, is shown in Figure 6. The image is taken with a reference signal at 45kHz. Apart from the two delaminations, one can see again the slight distortion of the fringe pattern between them, which indicates the lack of good adhesion between the skins and the core. Figure 6. Fringe pattern of the sandwich plate excited with a piezoelectric transducer at 25kHz and a shaker at 20kHz. In order to compare the results presented above with other established techniques, we performed experiments with lock-in thermography on the plate B. A thermal wave is generated by means of uniform heat excitation (laser) which is highly attenuated. The penetration depth or thermal diffusion length is proportional to the thermal diffusivity of the material and inversely proportional to the frequency of excitation. The contrast originates from the difference in the thermal resistance of the inclusion with respect to the bulk material. In Figure 7, one can see the images obtained at three different frequencies: 0.1, 0.068 and 0.05Hz. Both amplitude and phase are depicted although for practical applications, phase angle imaging is preferable due to its insensitivity to variable surface emissivity and non uniformity of heating and/or optical absorption. Evidently and expectedly, the results show that the metallic inclusions provide higher contrast due to the great difference of its thermal properties with respect to the ones of the PMI and the composite. On the other hand, poor contrast is obtained in such a case for the pure, closed or open air gaps or Teflon pieces. This is normal as the thermal resistance of Teflon is very similar to the one of PMI and/or air. (a) (b) (c) Figure 7. Amplitude (upper) and phase (lower) images of the thermal wave at (a) 0.1, (b) 0.068 and (c) 0.05Hz. Conclusions-Discussion The increasing demands of the industrial world for efficient and fast (full-field) NDT methods led us to investigate and compare the results obtained with two competitive methods. Both methods, shearography and lock-in thermography are highly applicable in the industrial field due to their compactness and ease of use. The images obtained with shearography are rather more difficult to interpret but the outcome of the investigation is that the two methods have different potential. While shearography is more suited to evaluate delaminations, even when they are closed, in the linear or nonlinear regime, lock-in thermography is rather better in the detection of inclusions with high thermal resistance contrast. In the latter case, shearography typically provides no result because (depending of course on the dimensions of the inclusion) the influence on the vibration characteristics is too small. On the other hand, lock-in thermography is less sensitive to delaminations between the skin and the core of a sandwich material due to the similarities of the thermal diffusivity of air and the underlying foam. 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