Impact of System Nonlinearities on Output-Based Whirl Flutter Prediction

SM-2024-TVF-5096

2/6/2024

Authors
Abstract
Content

This paper investigates the impact of system nonlinearities on output-based whirl flutter prediction. The investigation considers four widely-used damping identification and extrapolation methods-logarithmic decrement, exponential fit, matrix-pencil estimation, and moving-block analysis-alongside bifurcation forecasting, a recently proposed method. The examined methods are compared by predicting the whirl flutter speed of a propeller-nacelle system with structural nonlinearities using computational output data. The comparisons consider various hardening and softening behaviors, excitation amplitudes, and pre-flutter forward speeds, including values as low as 30% below the flutter point. Results indicate that all methods accurately predict the whirl flutter speed for weak nonlinearities and small-amplitude perturbations. While the first four methods markedly lose accuracy with stronger nonlinear effects, bifurcation forecasting maintains consistent accuracy across all examined conditions, even when significant nonlinearities are present.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM-2024-TVF-5096
Citation
Riso, C., "Impact of System Nonlinearities on Output-Based Whirl Flutter Prediction," Sixth Decennial VFS Aeromechanics Specialists Conference, Santa Clara, California, Feb 2024, Santa Clara, California, February 6, 2024, https://doi.org/10.4050/SM-2024-TVF-5096.
Additional Details
Publisher
Published
2/6/2024
Product Code
SM-2024-TVF-5096
Content Type
Technical Paper
Language
English