This paper delves into the thermo-mechanical behavior of clamped composite laminated arches exposed to non-uniform thermal environments. Exact solutions for temperature, displacements, and stresses in laminated arches with arbitrary thickness and number of layers are derived based on the theory of thermoelasticity. Given the complexity of the inhomogeneous temperature conditions at the edges, a specialized temperature function is constructed to accurately satisfy the non-homogeneous thermal boundary conditions. On the basis of Fourier’s law of heat conduction and the principle of superposition, the analytical temperature solution is obtained with the transfer matrix method. Clamped support conditions are addressed by incorporating unit pulse functions and Dirac delta functions into the analysis. The state equation is established with displacements and stresses serving as the state variables. According to the continuity conditions at the interfaces and the mechanical conditions on the surfaces of the laminated arch, the exact solutions for displacements and stresses are uniquely determined. The convergence and comparison studies confirm the efficacy and accuracy of the proposed method. Furthermore, three detailed numerical examples are presented to explore the effects of surface temperature, thickness-to-radius ratios, material properties, and layer numbers on the distributions of temperature, displacements, and stresses within the laminated arches.
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