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Numerical implementation results and features of optimal size-weight project for composite stringer aircraft panels with restrictions according to refined buckling theory

Crossref DOI link: https://doi.org/10.1007/s42401-025-00402-9

Published Online: 2025-10-17

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

Authors

Korolskii, V. V.

Gavva, L. M. https://orcid.org/0009-0008-7347-334X
Funding

Funding for this research was provided by:

Ministry of Science and Higher Education of the Russian Federation (Grant agreement of April, 20, 2022 № 075-15- 2022-309)
License Information

Text and Data Mining valid from 2025-10-17

Version of Record valid from 2025-10-17
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Article History

Received: 7 April 2025

Revised: 11 August 2025

Accepted: 15 August 2025

First Online: 17 October 2025

Declarations

:

: Not applicable.

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