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Thermal buckling analysis of laminated composite beams using hyperbolic refined shear deformation theory
Authors:Mokhtar Bouazza  Noureddine Benseddiq  Ashraf M. Zenkour
Affiliation:1. Department of Civil Engineering, University of Bechar, Bechar, Algeria;2. Laboratory of Materials and Hydrology (LMH), University of Sidi Bel Abbes, Sidi Bel Abbes, Algeria;3. Mechanics Laboratory of Lille, CNRS UMR 8107, University of Lille 1, Villeneuve d’Ascq, France;4. Department of Mathematics, Faculty of Science, King Abdulaziz University, Jeddah, Saudi Arabia;5. Department of Mathematics, Faculty of Science, Kafrelsheikh University, Kafrelsheikh, Egypt
Abstract:In this article, thermal buckling of laminated composite beams, based on hyperbolic refined shear deformation theory, presented for the first time, is formulated using the principle of minimum total potential energy. Navier’s analytical solution is derived to analytically solve the differential equations and the thermal critical buckling is presented in closed-form solution. The effects of temperature distribution, length to thickness ratio, modulus ratio, and thermal expansion coefficient ratio on thermal buckling of isotropic, orthotropic and laminated composite beams are investigated. The accuracy of the numerical model is verified by comparison with the available results in the literature.
Keywords:Analytical solution  beam  hyperbolic-refined shear deformation theory  thermal buckling
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