To address the lack of research on the traveling wave vibration characteristics of rotating composite honeycomb sandwich cylindrical shells, this study proposes a semi-analytical model. The model is formulated based on the first-order shear deformation theory, the Ritz method, the domain decomposition method, and Jacobi orthogonal polynomials, aiming to predict both the natural frequencies and the forward and backward traveling wave frequencies under rotational conditions. The key model parameters are systematically determined through convergence analysis. The accuracy of the model is validated through comparisons with existing research cases and experimental test results. The results show that the model corresponds well with the results in the corresponding literature, and the maximum error between the model and the experimental results is 5.5 %. Furthermore, the effects of boundary stiffness loss and thickness ratio on the rotational traveling wave vibration frequencies, modal step regions, and critical rotational speeds are examined. The results show that the change of rotational speed will lead to complex frequency steering and modal shape exchange. In the high-order mode, the sensitivity of the frequency turning point to the boundary stiffness and speed decreases. In addition, properly increasing the thickness ratio of fiber layer can help to improve the structural stiffness.
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