Turkish Journal of Engineering

Yazarlar: Ali DOĞAN

Konular:Mühendislik

DOI:10.31127/tuje.665156

Anahtar Kelimeler:Buckling Analysis

Özet: This paper investigates the buckling analysis of symmetrically thin and thick composite plates. Using the Hamilton’s principle, the governing equation for thin and thick composite plates is derived. The equation of motion for thin and thick laminated rectangular plates subjected to in-plane loads is obtained with the help of Hamilton’s principle. Considering the Navier solution technique, closed form solutions are attained and buckling loads are found by solving the eigenvalue problems. Results of the numerical studies for the buckling of laminated composite plates (LCP) are demonstrated and benchmarked with former studies in the literature and ANSYS finite element methods.

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