A generalised power-law formulation for the modelling of damping and stiffness nonlinearities. (15th May 2021)

• Record Type: Journal Article
• Authors: Civera, Marco; Grivet-Talocia, Stefano; Surace, Cecilia; Zanotti Fragonara, Luca
• Is Part Of: Mechanical systems and signal processing. Volume 153(2021)
• Publication Date: 2021-05-15
• Subjects: Nonlinear dynamics -- Nonlinear hardening -- Nonlinear damping -- Large vibrations -- Nonlinear system identification -- High-Aspect-Ratio wing; Structural dynamics -- Periodicals; Vibration -- Periodicals; Constructions -- Dynamique -- Périodiques; Vibration -- Périodiques; Structural dynamics; Vibration; Periodicals; 621
• DOI: 10.1016/j.ymssp.2020.107531
• Languages: English
• ISSNs: 0888-3270

Abstract

Highlights: An analytical SDoF model with nonlinear stiffness and damping terms is introduced. The model is applied to the large oscillations of a prototype wing. The model parameters are calibrated in the steady state frequency domain. The model calibration accounts for different levels of input energy. Different structural conditions (with additional masses) are considered. Abstract: In this paper, a single-degree-of-freedom dynamic model is described, with displacement- and velocity-dependent nonlinearities represented by power laws. The model is intended to support the dynamic identification of structural components subjected to harmonic excitation. In comparison to other analytical expressions, the data-driven estimation of the nonlinear exponents provides a large versatility, making the generalised model adaptable for a wide number of different nonlinearities in both stiffness and damping. For instance, the proposed damping formulation can naturally accommodate air drag (quadratic) damping as well as dry friction. Differently to purely data-driven methods (e.g. black boxes), the obtained model is fully inspectable. The proposed formulation is here applied to the large oscillations of a prototype highly flexible wing and fitted on its steady state response in the frequency domain. These large-amplitude flap-wise bending oscillations are known to be affected by nonlinearities in both the stiffness (nonlinear hardening) and the velocity-dependent damping terms. The model is validated against experiments for different structural configurations and input amplitudes, as both these nonlinearities are energy-dependent.