“…The web and flanges tapering parameters, the load height position, internal bending moment, and boundary conditions are the main factors affecting the lateral-torsional buckling strength of thin-walled beams with varying cross-section. 1,2,9,10 With the development in high technology and fabrication processes, the practical applications of thin-walled laminate composite structural components have been extensively come into vogue in many advanced and innovative engineering systems such as axles of vehicles, space structures, helicopter rotors, wind turbine blades, and aircraft wings. The main reason for this increase is the conspicuous features 1 of fiber-reinforced composite materials, for instance, high fatigue resistance, durability, corrosion resistance, and high stiffness-to-weight and strength-to-weight ratios.…”