Priyanka, R.Jeyaraj, J.2026-02-042022Composite Structures, 2022, 281, , pp. -2638223https://doi.org/10.1016/j.compstruct.2021.115028https://idr.nitk.ac.in/handle/123456789/22688This paper explores the buckling and free vibration behaviors of micro laminated composite beams (MLCBs) exposed to varying axial loads using the modified couple stress theory (MCST), with arbitrary boundary conditions and layups. The size effect is captured in MCST by taking into account the material length scale parameters. In the axial direction, the applied load has either constant, linear, or parabolic variations. The equilibrium equations are derived and solved using Hamilton's principle and Ritz method respectively. The size effect is observed to be more pronounced when the thickness of the beam is similar to the material length scale parameter, and it nearly vanishes as the beam thickness increases. The small size effect variation is different for different boundary conditions. For parabolically increasing loading case, the rate of reduction of the fundamental frequency with an increase in applied load intensity is greater compared to other loadings. © 2021 Elsevier LtdAxial loadsBoundary conditionsComposite beams and girdersLaminated compositesLaminatingShear flowBucking and free vibrationComposite beamDeformation theoryFree vibrationMicro composite beamMicrocompositeModified couple stress theoriesNormal deformationsRitz methodsShear and normal deformation theorySizes effectSize determination