4.7 Article

GA Optimization of Variable Angle Tow Composites in Buckling and Free Vibration Analysis through Layerwise Theory

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AEROSPACE
卷 8, 期 12, 页码 -

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MDPI
DOI: 10.3390/aerospace8120376

关键词

variable angle tow; layerwise theory; genetic algorithm optimization; buckling; free vibration; surrogate model; response surface

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In this research, variable angle tow composites were utilized to enhance the buckling and vibration behavior of structures. The approach involved employing a 1D CUF and GA optimization method, with the effectiveness of the GA approach confirmed through the use of the RS method. The results demonstrated a cost reduction in optimized VAT performance through GA optimization, and the applicability of LHS sampling for future research stages was also confirmed.
In the current research, variable angle tow composites are used to improve the buckling and free vibration behavior of a structure. A one-dimensional (1D) Carrera Unified Formulation (CUF) is employed to determine the buckling loads and natural frequencies in Variable Angle Tow (VAT) square plates by taking advantage of the layerwise theory (LW). Subsequently, the Genetic Algorithm (GA) optimization method is applied to maximize the first critical buckling load and first natural frequency using the definition of linear fiber orientation angles. To show the power of the genetic algorithm for the VAT structure, a surrogate model using Response Surface (RS) method was used to demonstrate the convergence of the GA approach. The results showed the cost reduction for optimized VAT performance through GA optimization in combination with the 1D CUF procedure. Additionally, a Latin hypercube sampling (LHS) method with RS was used for buckling analysis. The capability of LHS sampling confirmed that it could be employed for the next stages of research along with GA.

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