This master’s thesis investigates the steady aeroelastic behavior of an open-rotor configuration, focusing on the interaction between structural deformations and aerodynamic loads. A comprehensive framework is developed to predict the rotor system’s aeroelastic response. The methodology combines structural and aerodynamic analyses. Structural modeling employs a Reduced-Order Model (ROM) to efficiently capture overall behavior, and a detailed modal analysis is conducted, examining vibration modes and the influence of material properties. The effect of Young’s modulus on natural frequencies is examined through numerical simulations, and a Campbell diagram is produced to depict their variation with rotational speed. Aerodynamic loads are computed using the Vortex Particle Method (VPM) and a lifting-line approach for the considered open-rotor configuration.