Investigation of the mechanical properties of nanocomposites with multi-wall carbon nanotube reinforcement and carbon fiber/epoxy

In this study, the focus is on exploring remarkable world of aircraft structures with aim creating a material that pushes boundaries and garners global attention. The successful formulation composite investigated by skillfully manipulating weight quantity ratios. To achieve desired outcome, different ratios multi-walled carbon nanotubes (MWNTs), specifically 8g 16g, are combined. Furthermore, these MWNTs proportionately mixed epoxy in volumes 200ml, 400ml, 600ml, 800ml, following valence equation correlates gram ratio epoxy. For purpose ensuring homogeneity facilitating optimal component blending, an electric convector magnetic core employed to generate vortices, aiding thorough mixing constituents. Subsequently, mixture hardened after proper placement. Prior casting, introduction hardener, whether its liquid state or incorporating reinforcement layers nanofibers (ranging from 0 16 layers), enhances fortifies properties material. ingenuity approach showcased exceptional results obtained evaluation tensile stress impact. Through rigorous testing meticulous analysis, findings validate theoretical foundation upon which endeavor built, underscoring success innovative concept.