📣 Help Shape the Future of UKRI's Gateway to Research (GtR)

We're improving UKRI's Gateway to Research and are seeking your input! If you would be interested in being interviewed about the improvements we're making and to have your say about how we can make GtR more user-friendly, impactful, and effective for the Research and Innovation community, please email gateway@ukri.org.

Model identification of a fluttering aerofoil using control-based continuation and normal form analysis (2020)

First Author: Lee K.H.

Attributed to: Next-generation test methods for nonlinear structures funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Publication URI: https://api.elsevier.com/content/abstract/scopus_id/85105797672

Type: Other

Parent Publication: Proceedings of ISMA 2020 - International Conference on Noise and Vibration Engineering and USD 2020 - International Conference on Uncertainty in Structural Dynamics