Abstract
A model of a rigid rotor system under axial thrust with rotor-to-stator is developed based on the classic impact theory and is analyzed by the Lagrangian dynamics. The rubbing condition is modeled using the elastic impact-contact idealization, which consists of normal and tangential forces at the rotor-to-stator contact point. Mass eccentricity and rotating speed are used as control parameters to simulate the response of rotor system. The motions of periodic, quasi-periodic and chaotic are found in the rotor system response. Mass eccentricity plays an important role in creating chaotic phenomena.
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An, X., Zhou, J., Xiang, X. et al. Dynamic response of a rub-impact rotor system under axial thrust. Arch Appl Mech 79, 1009–1018 (2009). https://doi.org/10.1007/s00419-008-0274-x
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DOI: https://doi.org/10.1007/s00419-008-0274-x