Buckling,collapse and failure analysis of FRP sandwich panels |
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| Affiliation: | 1. Applied Physics Laboratory, The Johns Hopkins University, 11100 John Hopkins Road, Laurel, MD 20723-6099, USA;2. Department of Mechanical Engineering, The Johns Hopkins University, 11100 John Hopkins Road, Laurel, MD 20723-6099, USA;3. The United States Naval Academy, 121 Blake Road, Annapolis, MD 21402-5000, USA;1. School of Civil Engineering, University of South China, Hunan, Hengyang 421001, China;2. Hunan Provincial Key Laboratory of High Performance Special Concrete, Hunan, Hengyang 421001, China;3. China Nuclear Construction Key Laboratory of High Performance Concrete, Hunan, Hengyang 421001, China;4. Xi ''an Branch of Chengdu JZFZ Architectural Design Co., LTD, 710000, China;5. School of Electric Power, Civil Engineering and Architecture, Shanxi University, Shanxi, Taiyuan 030013, China;1. Department of Civil, Construction, and Environmental Engineering, Iowa State University, Ames, IA 50011, USA;2. Department of Civil Engineering, University of Idaho, Moscow, ID 83844, USA;1. Research Institute for Materials Science and Technology (INTEMA), Universidad Nacional de Mar del Plata, CONICET, Av. Juan B. Justo 4302, B7608FDQ Mar del Plata, Argentina;2. Institute of Lightweight Structures, Universität der Bundeswehr München, Werner-Heisenberg-Weg 39, 85577 Neubiberg, Germany;2. Composite Construction Laboratory (CCLab), École Polytechnique Fédérale de Lausanne, BP 2225, Station 16, CH-1015 Lausanne, Switzerland |
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| Abstract: | Rectangular orthotropic fiber-reinforced plastic (FRP) sandwich panels were tested for buckling in uni-axial compression. The panels, with 0.32 cm (0.125 in.) face sheets and a 1.27 cm (0.5 in.) core of either balsa or linear poly(vinyl chloride) (PVC) foam, were tested in two sizes: 154×77 cm2 (72×36 in.2) and 102×77 cm2 (48×36 in.2). The sandwich panels were fabricated using the vacuum-assisted resin transfer molding process. The two short edges of the sandwich panels were clamped, while the two long edges were simply supported for testing. The clamped panel ends were potted into a steel frame. The experimental elastic buckling loads were then measured using strain gauges fixed to both sides of the panels. A total of 12 panels were tested under uni-axial compression. Bifurcation in the load versus engineering strain curve was noted in all cases. For all six sandwich panels tested using balsa core, the type of failure was easily identified as face sheet delamination followed by core shear failure. For all six PVC foam core sandwich panels tested, the type of failure consisted of core shear failure with little or no face sheet delamination. In the failed balsa core panels there was little or no evidence of balsa remaining on the FRP face sheet, however, in the PVC foam core panels there were ample amounts of foam left on the FRP face sheet. It was concluded that although the buckling loads for the foam core panels were not as high as those for the balsa core panels, PVC foam core bonding to the FRP face sheets was superior to balsa core bonding. |
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