In the present investigation the fatigue behaviour of carbon fibre reinforced plastic laminates under realistic service loading conditions has been examined, Laminates with different lay-up sequences have been tested for fatigue under spectrum loading with three different peak load levels. The damage in the laminates was characterized by using ultrasonic C-Scan as well as dynamic mechanical analysis and the damage mechanism was analyzed using scanning electron microscope. A similar investigation was also conducted on laminates with a hole. The results indicate that the spectrum loading did affect the modulus and fibre/matrix interfacial properties of all type of laminates investigated and also caused delamination in the laminate with a hole due to stress concentration around the hole. (c) 2008 Elsevier B.V. All rights reserved.
机构:
Univ Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USAUniv Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USA
Choi, SW
;
Hahn, HT
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机构:Univ Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USA
Hahn, HT
;
Shyprykevich, P
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h-index: 0
机构:Univ Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USA
机构:Slovak Acad of Sciences, Inst of, Materials & Machine Mechanics,, Bratislava, Czech, Slovak Acad of Sciences, Inst of Materials & Machine Mechanics, Bratislava, Czech
机构:
Univ Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USAUniv Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USA
Choi, SW
;
Hahn, HT
论文数: 0引用数: 0
h-index: 0
机构:Univ Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USA
Hahn, HT
;
Shyprykevich, P
论文数: 0引用数: 0
h-index: 0
机构:Univ Calif Los Angeles, Dept Mech & Aeronaut Engn, Los Angeles, CA 90095 USA
机构:Slovak Acad of Sciences, Inst of, Materials & Machine Mechanics,, Bratislava, Czech, Slovak Acad of Sciences, Inst of Materials & Machine Mechanics, Bratislava, Czech