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Growing Science » Tags cloud » Hybrid composites

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1.

3D multi-objective optimization of hybrid composite laminates: Influence of fiber orientation and stacking sequence Pages 199-216 PDF Download PDF

Authors: Ibrahim Beroual, Moussa Amadji, Djamel Haddad

doi 10.5267/j.esm.2026.2.002

🔑 Keywords: Genetic algorithm, Hybrid composites, Optimization, Finite element method (FEM), ANSYS

Abstract:
Hybrid laminated composites, integrating High Strength (HS) carbon and glass fibers (E, S) within an epoxy matrix, deliver an optimal compromise between lightweight design, mechanical strength, and cost-effectiveness for applications in industrial, aerospace, automotive, and civil engineering sectors. This study presents a three-dimensional optimization of mechanical performance through a multi-objective genetic algorithm (MOGA) under static loading conditions. The design variables encompass the number of plies (6 to 12), fiber orientation angles (-90°≤ θ ≤90°), and ply materials: HS-Carbon/Epoxy (CF-EP), E-Glass/Epoxy (EG-EP) and S-Glass/Epoxy (SG-EP). A constraint mandating 25% CF-EP placement at the core to maximize stiffness while minimizing stresses. The objectives are to enhance the longitudinal modulus (Ex) and reduce von-Mises stress, while ensuring compliance with the Tsai-Wu failure criterion. An analytical model, implemented in MATLAB, incorporates stiffness matrices, Tsai-Wu failure indices, and von-Mises stress calculations, demonstrating a 30% increase in stiffness and effective mitigation of stress concentrations through centralized CF-EP placement. These findings are corroborated by finite element method (FEM) simulations conducted in ANSYS, which exhibit strong agreement with analytical predictions. This hybrid methodology offers a strong framework for developing high-performance laminated composites, significantly impacting applications requiring structural reliability and efficiency.
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Journal: ESM | Year: 2026 | Volume: 14 | Issue: 2 | Views: 760

 
2.

Nonlinear forced vibration of hybrid composite rectangular plates Pages 209-228 PDF Download PDF

Authors: Alireza Shooshtari, Soheil Razavi

doi 10.5267/j.esm.2014.4.002

🔑 Keywords: Analytical modeling, Hybrid composites, Nonlinear forced vibration

Abstract:
In the present study, the nonlinear forced vibration of symmetric laminated rectangular plates, including Glare fiber metal laminated rectangular plate, is investigated based on the first order shear deformation theory. The boundary condition is considered to be immovable simply support. The Galerkin method is used to obtain the nonlinear ordinary differential equation in terms of an unknown time function. The obtained equation is solved analytically by the multiple time scales method. The obtained results are compared with the numerical solution of the nonlinear ordinary differential equation of motion and a good agreement is found between them.
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Journal: ESM | Year: 2014 | Volume: 2 | Issue: 3 | Views: 3180

 

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