A micromechanical modeling procedure is developed to predict the viscoelastic properties of a graphite nanoplatelet/epoxy composite as a function of volume fraction and nanoplatelet diameter. The predicted storage and loss moduli from the model are compared to measured values from the same material using Dynamical Mechanical Analysis, nanoindentation, and tensile tests. In most cases, the model and experiments indicate that for increasing volume fractions of nanoplatelets, both the storage and loss moduli increase. Also, in most cases, the model and experiments indicate that as the nanoplatelet diameter is increased, the storage and loss moduli decrease and increase, respectively
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of their high-specific stiffness, carbon-filled epoxy composites can be used in structural c...
A micromechanical modeling procedure is developed to predict the viscoelastic properties of a graphi...
In order to facilitate the interpretation of experimental data, a micromechanical modeling procedure...
To facilitate the interpretation of experimental data, a micromechanical modeling procedure is devel...
In order to facilitate the interpretation of experimental data, a micromechanical modeling procedure...
Structural components of modern aircraft, such as the fuselage and control surfaces, are commonly co...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of their high-specific stiffness, carbon-filled epoxy composites can be used in structural c...
A micromechanical modeling procedure is developed to predict the viscoelastic properties of a graphi...
In order to facilitate the interpretation of experimental data, a micromechanical modeling procedure...
To facilitate the interpretation of experimental data, a micromechanical modeling procedure is devel...
In order to facilitate the interpretation of experimental data, a micromechanical modeling procedure...
Structural components of modern aircraft, such as the fuselage and control surfaces, are commonly co...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of the relatively high specific mechanical properties of carbon fiber/epoxy composite materi...
Because of their high-specific stiffness, carbon-filled epoxy composites can be used in structural c...