This paper addresses the dynamics of locally-resonant sandwich beams, where multi-degree-offreedom viscously-damped resonators are periodically distributed within the core matrix. Using an equivalent single-layer Timoshenko beam model coupled with mass-spring-dashpot subsystems representing the resonators, two solution methods are presented. The first is a direct integration method providing the exact frequency response under arbitrary loads. The second is a complex modal analysis approach obtaining exact modal impulse and frequency response functions, upon deriving appropriate orthogonality conditions for the complex modes. The challenging issue of calculating all eigenvalues, without missing anyone, is solved applying a recently-introduced contour-integral algorithm to a characteristic equation built as determinant of an exact frequency-response matrix, whose size is 4 × 4 regardless of the number of resonators. Numerical applications prove exactness and robustness of the proposed solutions.Recently, the concept of locally-resonant beam has been proposed also for sandwich beams, which are ideally suitable to host small resonators within the core matrix, featuring single or multiple degrees of freedom (DOFs). Pioneering work in this field is due to Sun and co-workers [10,[19][20][21][22][23][24]. They proposed an equivalent single-layer Timoshenko beam model coupled with mass-spring subsystems representing the resonators, investigating the dynamic behaviour under different excitations, including impact [21] and moving ones [23]. The mass-spring subsystems were considered as exerting point forces [19,20] or distributed forces over the mutual distance [10,19]. The equivalent single-layer