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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