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Property Evaluation of FML (Glare)
Abstract:
Fiber metal laminate (Glare) made of 2014-T6 aerospace aluminum alloy sheets adhesively bonded with E-glass fiber based composite prepregs is investigated in the paper. The fabrication procedure of the laminate is explained. Chemical composition, macrostructure and residual stress of aluminum alloy are obtained. Mechanical properties of the laminate viz. tensile, flexural and shear strengths are measured.
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212-216
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February 2021
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© 2021 Trans Tech Publications Ltd. All Rights Reserved
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