Evaluation of a time-varying mass nonlinear energy sink on the helicopter ground resonance problem
Author:
Affiliation:
1. Universidade Federal de Uberlandia
2. ISAE-SUPAERO
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-4395
Reference17 articles.
1. Helicopter Ground Resonance Phenomenon With Blade Stiffness Dissimilarities: Experimental and Theoretical Developments
2. Response and instability prediction of helicopter dynamics on the ground
3. Bergeot, B., Bellizzi, S., and Cochelin, B. "Analysis of steady-state response regimes of a helicopter ground resonance model including a non-linear energy sink attachment," Vol.78, pp.72-89. https://doi.org/10.1016/j.ijnonlinmec.2015.10.006,URLhttps://linkinghub.elsevier.com/retrieve/pii/S0020746215002000.
4. Huang, J., and Zhou, X. "A time-varying mass metamaterial for non-reciprocal wave propagation," Vol.164, pp.25-36. https://doi.org/10.1016/j.ijsolstr.2018.12.029,URLhttps://linkinghub.elsevier.com/retrieve/pii/S0020768318305262.
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