Aerodynamics and vibration analysis of a helicopter rotor blade
Author:
Funder
Louisiana Space Grant Consortium
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s00707-024-03871-9.pdf
Reference49 articles.
1. Zhou, X., He, S., Dong, L., Atluri, S.N.: Real-time prediction of probabilistic crack growth with a helicopter component digital twin. AIAA J. 60(4), 2555–2567 (2022). https://doi.org/10.2514/1.J060890
2. Kang, Y., Cao, S., Hou, Y., You, Z., Ma, Q.: Analysis of backward whirl characteristics of rubbing dual-rotor systems. Acta Mech. 46, 1–31 (2023). https://doi.org/10.1007/s00707-023-03660-w
3. Bardera Mora, R., Matías García, J.C.: Helicopter rotor ground effect and frigate interaction investigated by particle image velocimetry. AIAA J. 60(1), 129–143 (2022). https://doi.org/10.2514/1.J060439
4. Sarker, P., Chakravarty, U.K.: On the dynamic response of a hingeless helicopter rotor blade. Aerosp. Sci. Technol. 115, 106741 (2021). https://doi.org/10.1016/j.ast.2021.106741
5. Patterson, R.P., Friedmann, P.P.: Vibration reduction on helicopter rotors using open-loop flow control. AIAA J. 60(1), 113–128 (2022). https://doi.org/10.2514/1.J060717
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