Crossmark

Semi-Analytical Study by Nonlinear Substructure Method Based on Frequency Response Functions to Determine Folding Wing Dynamic Behavior with Nonlinear Effects

Crossref DOI link: https://doi.org/10.1007/s40799-025-00775-8

Published Online: 2025-02-10

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Ghadimi, M.

Azarafza, R. https://orcid.org/0000-0002-7957-3295
Davar, A.

Eskandari Jam, J.
License Information

Text and Data Mining valid from 2025-02-10

Version of Record valid from 2025-02-10
More Information

Article History

Received: 30 June 2024

Accepted: 6 January 2025

First Online: 10 February 2025

Declarations

:

: The authors have no competing interests or no conflict of interest to declare that are relevant to the content of this article.

Document is current

Any future updates will be listed below