Full-field experimental analysis of a sandwich beam under bending and comparison with theories
Introduction
Sandwich plates and beams can be found in many engineering structures such as ships, bridges, planes, wind turbines, and other structures. Modern sandwich construction usually consists of two stiff face sheets and a soft middle core. Such a construction has a very advantageous weight to stiffness ratio. Research efforts devoted to sandwich structures have a long history [1]. Most investigations are either theoretical or numerical in nature [2], [3], [4], [5], [6], [7], [8], [9], [10], [11], [12], [13]. Of particular interest in these papers are the work of Kardomateas et al. [4], [5], in these studies, a formulation of the Elasticity solution for the behavior of sandwich beams is presented, then in a following study, the Extended High-Order Sandwich Panel Theory (EHSAPT) is formulated and compared with existing theories of composite sandwich beams. In Kardomateas et al. [6] the authors developed a Finite Element Model (FEM) based on EHSAPT, yielding results that were nearly identical to the analytical solution. Numerous studies have been performed on the bending behavior of composite sandwich beams [3], [12], [13], [14], [15], [16], [17], [18], [19], [20], [21], [22], [23], [24]. Though relatively few experimental investigations have investigated the validity for the numerous existing numeric models and analytic theories. There seems to be a disconnect between theory/numerical studies and experimental investigations in that very little efforts are devoted to checking each other’s results. Most studies, either theoretical/numerical or experimental, place emphasis on the global deformation (deflection) of a plate or beam, even though the dominant failure mode of a sandwich structure is the excessive deformation of the core [21], [22], [23], [24], [25], [26], [27], [28], [29], [30], [31], [32], [33], [34], [35]. The first full-field mapping of a sandwich core deformation is given by Gdoutos et al who employed the in-plane moiré method to mapping the core deformation [20]. With the advent of modern full-field measurement techniques, such a DIC (Digital Image Correlation), DSP (Digital Speckle Photography), DSC (Digital Speckle Correlation) more detailed deformation patterns of the core can be obtained. An example is the work of Fathi, Keller, and Altstaedt [36] in which the shear strain field of the foam core was calculated. In this paper, we present the results of a sandwich beam under three point-bending using DIC to obtain its displacement field and then calculate the strain fields using different displacement–strain relations, that model the linear or nonlinear behavior of elements of a composite sandwich beam, in accordance with the formulations developed by Yuan et al. [37].
In recent years there has been a rich outpouring of theoretical/numerical papers dealing with the deflection of sandwich plates/beams under bending [4], [5], [6], [7], [8], [9]. But no experimental effort, to the best of our knowledge, has been devoted to checking these models to ascertain which of the models matches with reality. In this paper, we present some experimental results in an effort to shed light on the validity of various theoretical/numerical models.
Section snippets
Materials
The composite sandwich structure was constructed using two woven carbon fiber face sheets with a compliant foam core. The core has a Young’s modulus of 40 MPa, a Poisson’s ratio of 0.18, and a shear modulus of 16.95 MPa. The woven carbon fiber sheets have a Young’s modulus of 21 GPa. The face sheets are adhered to the foam core with 3M™ Scotch-Weld™ Epoxy Adhesive DP420. The face sheets have a thickness of 1.25 mm and the core thickness is 32.25 mm, resulting in the total height of the specimen
Experimental procedures
The specimen was loaded in an MTS machine under a quasi-static loading with a displacement-controlled load speed of 0.05 mm/minute. A circular cylinder of 3.175 mm diameter was used for both the load and the supporting points to reduce the stress concentration that would have resulted if a narrow wedge type device were used for load and support. The supporting points are 254 mm apart to match the span of specimens from Kardomateas et al. [4], [5], [6]. A two-point fiber optic light source was
Results
The global load–deflection curve is given in Fig. 2. In which it shows that the beam first deformed essentially linearly and then turned into nonlinear. We recorded the digital image of the beam at every 100 N load interval and analyzed the deformation of the core thoroughly at 100 N, 200 N, 300 N, 400 N, 500 N, 600 N, 700 N, and 1000 N. Gdoutos et al. [21] characterized the nonlinear behavior of composite sandwich beams loaded in 3-point bending; A brief explanation of their theory is adapted
Discussion and conclusion
We have produced full field deformation patterns of a sandwich beam with two stiff face-sheets and a soft foam core loaded by three-point bending. We find that the voids in the foam core can be treated as speckles with judicious illumination. Using a DIC program, full field displacement distributions are obtained. In-plane strain fields using four different strain–displacement relationships are calculated and compared. We find that the strain patterns of all of them are essentially similar
CRediT authorship contribution statement
Austin Giordano: Conceptualization, Methodology, Data curation, Formal analysis, Visualization, Investigation, Validation, Writing - original draft, Writing - review & editing. Lingtao Mao: Conceptualization, Funding acquisition, Software, Writing - review & editing. Fu-Pen Chiang: Conceptualization, Methodology, Funding acquisition, Resources, Writing - review & editing, Supervision.
Declaration of Competing Interest
The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
Acknowledgements
The work was supported by ONR grant # N00014-17-1-2873 and the Chinese Natural Science Foundation #51374211. We would like to thank Dr. Yapa Rajapakse, Director of the US Office of Naval Research’s Solid Mechanics Program, for his support over the years for the advancement of the speckle technique.
Data Availability Statement
The raw/processed data required to reproduce these findings cannot be shared at this time as the data also forms part of an ongoing study.
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