Usage of composite materials like Fibre Reinforced Plastics for structural applications has been increasing in recent years. Delamination of adhesively bonded composite joints is a concern as it causes premature failure of the bond. A technique to reduce delamination in CFRP single lap joints (SLJs) by inserting additional adhesive layers in the adherends is analyzed for quasi-static and impact conditions, with satisfactory results. For quasi-static conditions failure by delamination is avoided, while for a low velocity impact scenario its onset is delayed. In both cases the failure load is increased. A numerical model using finite element analysis is developed in ABAQUS to study the performance of the best configuration. Experimental and numerical results are compared.
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Kocaeli Univ, Fac Aeronaut & Astronaut, Aviat Mat Res & Dev Lab, TR-41285 Kocaeli, TurkeyKocaeli Univ, Fac Aeronaut & Astronaut, Aviat Mat Res & Dev Lab, TR-41285 Kocaeli, Turkey
Akman, Erhan
Erdogan, Yalcin
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Kocaeli Univ, Elect Opt Syst Engn, TR-41380 Kocaeli, TurkeyKocaeli Univ, Fac Aeronaut & Astronaut, Aviat Mat Res & Dev Lab, TR-41285 Kocaeli, Turkey
Erdogan, Yalcin
Bora, Mustafa Ozgur
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Kocaeli Univ, Fac Aeronaut & Astronaut, Aviat Mat Res & Dev Lab, TR-41285 Kocaeli, TurkeyKocaeli Univ, Fac Aeronaut & Astronaut, Aviat Mat Res & Dev Lab, TR-41285 Kocaeli, Turkey
Bora, Mustafa Ozgur
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Coban, Onur
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Oztoprak, Belgin Genc
Demir, Arif
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Kocaeli Univ, Dept Phys, TR-41380 Kocaeli, Turkey
KOU Technopk, BEAM Ar Ge Opt, Laser & Spect, TR-41275 Kocaeli, TurkeyKocaeli Univ, Fac Aeronaut & Astronaut, Aviat Mat Res & Dev Lab, TR-41285 Kocaeli, Turkey