On the effects of rotor induced vibrational stability on helicopter flight dynamics
Crossref DOI link: https://doi.org/10.1007/s13272-024-00718-w
Published Online: 2024-02-12
Published Print: 2024-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Saetti, Umberto https://orcid.org/0000-0003-0648-9540
Horn, Joseph F.
Berger, Tom
Text and Data Mining valid from 2024-02-12
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Article History
Received: 24 August 2023
Revised: 9 January 2024
Accepted: 15 January 2024
First Online: 12 February 2024
Declarations
:
: The authors have no competing interests to declare that are relevant to the content of this article.