Against the research background of rocket fairings, this study investigates the vibration characteristics and nonlinear dynamic behavior of two-phase braided composite truncated conical shells under complex environments. We establish a dynamic model via FSDT and Hamilton's principle, studying the two-phase braided composite truncated conical shell's natural vibration. FEA comparison shows ≤2.95 % error. Higher fiber volume boosts frequency and stiffness. Subsequently, we analyze the occurrence of 1:1 internal resonance when the half apex angle is 60° On this basis, external excitation, aerodynamic forces, and damping effects are introduced to further establish a nonlinear dynamic model. The Galerkin method is used to discretize the nonlinear governing equations, and the pseudo-arclength continuation method is used to analyze the effects of parameter variations on the 1:1 internal resonance behavior. The results reveal that increasing the fiber volume fraction, braiding angle, and damping can effectively reduce the resonance peak. Finally, we examine the nonlinear dynamic behavior of the structure, with a focus on revealing the mechanisms by which external excitation and damping affect the dynamic stability of the system. The results provide important theoretical support for the vibration control and structural reliability design of braided composite thin-walled components.
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