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