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Publication - Dr Ludovic Renson

    Nonlinear Phase Separation Testing of an Experimental Wing-Engine Structure

    Citation

    Renson, L, Noel, J, Barton, D, Neild, S & Kerschen, G, 2017, ‘Nonlinear Phase Separation Testing of an Experimental Wing-Engine Structure’. in: Rotating Machinery, Hybrid Test Methods, Vibro-Acoustics & Laser Vibrometry: Proceedings of the 35th IMAC, A Conference and Exposition on Structural Dynamics 2017. Springer, pp. 115-117

    Abstract

    Modal testing of nonlinear engineering structures is currently a research area that attracts substantial attention. Recently, a nonlinear generalisation of phase separation testing has been proposed for identifying nonlinear normal modes (NNMs) based on input and output measurements. The nonlinear phase separation (NPS) method integrates identification and continuation tools to calculate multiple NNMs from broadband data. The present contributionr reports the first experimental application of the NPS method. The structure of interest is a model inspired by a wing with two engines connected by means of nonlinear pylons with softening-hardening stiffness characteristics. The frequency-energy dependences of four NNMs in the 0-100 Hz range are estimated, including modal interactions. NNMs identified using the NPS method are also compared to free-decay testing results

    Full details in the University publications repository