Multi-Fidelity Analysis of a Composite Beam
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Abstract
The composite ply is made up of two basic components, the fiber and the matrix. The plies are placed together in a mold in a certain order to form a composite laminate. This study presents a method for analyzing the mechanical response of a composite beam from microscopic calculations of the fiber and the matrix. Through the micromechanics and the semi-empirical method to calculate the material properties of the composite ply, using the classical lamination theory (CLT) and the improved Tsai-Wu strength theory to calculate the properties of the composite laminate. Then, using the Euler-Bernoulli beam theory to calculate the mechanical response such as stress, displacement, and safety factor of the composite beam. The results are compared with the experimental results, showing a good agreement.
Keywords
composite beam, composite ply, classical lamination theory, laminate, strength
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