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In-plane shear properties of unidirectional glass fiber (U)/random glass fiber (R)/epoxy hybrid and non-hybrid composites
Authors:AI Selmy  AR Elsesi  NA Azab  MA Abd El-baky
Affiliation:1. Mechanical Design and Production Engineering Department, Faculty of Engineering, Zagazig University, Egypt;2. Production Engineering Department, Faculty of Engineering, El Monofiya University, Egypt;3. Mechanical Design and Production Engineering Department, Faculty of Engineering, Ein-Shams University, Egypt;1. DEMec, Faculdade de Engenharia, Universidade do Porto, Rua Dr. Roberto Frias, s/n, 4200-465 Porto, Portugal;2. INEGI, Universidade do Porto, Rua Dr. Roberto Frias, 400, 4200-465 Porto, Portugal;3. ISVOUGA — Instituto Superior de entre Douro e Vouga, Rua António de Castro Corte Real, Apartado 132, 4520-181 Santa Maria da Feira, Portugal;4. CIDEM/ISEP — Instituto Superior de Engenharia do Porto — Instituto Politécnico do Porto, Rua Dr. António Bernardino de Almeida, 431, 4249-015 Porto, Portugal;5. AIRBUS Operations GmbH, Kreetslag 10, 21129 Hamburg, Germany;1. Dept. of Aerospace Eng., Ryerson University, 350 Victoria St., Toronto, Canada M5B 2K3;2. Dept. of Mechanical and Industrial Eng., Ryerson University, 350 Victoria St., Toronto, Canada M5B 2K3;1. Industrial and Materials Science, Chalmers University of Technology, Hörsalsvägen 7A, SE-41296 Göteborg, Sweden;2. Composite Mechanics and Structures, DTU Wind Energy, Technical University of Denmark, Frederiksborgvej 399, DK-4000 Roskilde, Denmark
Abstract:The in-plane shear properties (shear strength τxy and shear modulus Gxy) of unidirectional glass fiber (U)/random glass fiber (R)/epoxy hybrid and non-hybrid composites have been investigated experimentally and theoretically. The effect of stacking sequence and random fiber relative volume fraction (VfR/VfT) in hybrid composites were reported. Laminates were fabricated by hand lay-up technique with a total of 5 plies, by varying the number and position of random glass layers so as to obtain four different hybrid laminates; i.e. 0.5R/U/U]S, U/0.5R/U]S, U/U/0.5R]S, and U/R/U/R/U]. All unidirectional fiber laminate U]5 and another of all random fiber laminate R]5 were also fabricated for comparison purpose. The average thickness of the manufactured laminates is 5.5 ± 0.2 mm and the total fiber volume fraction (VfT) is 37%. Failure modes of all specimens were investigated. Results indicated that the in-plane shear properties (shear strength τxy and shear modulus Gxy) of unidirectional fiber composite can be considerably improved by incorporation of random glass fiber and forming hybrid composites.
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