Abstract
Abstract The current study aims to investigate the mechanical behavior of Kevlar/carbon-epoxy composites, specifically their response to various mechanical stresses. These materials are intended for use as aircraft wing skins, making it crucial to understand their performance under different conditions. Several tests were conducted, including Inter delamination, Double Shear and Flexural, to assess the material’s ability to withstand these stresses. The hybrid composites have been set volume fraction ratio as 0.5. The obtained results were analyzed using NASTRAN analysis software. It was found that Kevlar/carbon composites exhibit high shear strength under ambient conditions, but the presence of notches significantly affects this property. Additionally, the flexural strength and resistance to compression failure were observed to vary accordingly.
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