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Parallelized complex method for multidisciplinary optimization of aeroelastic performance in thin-walled wing–engine system using bidirectional curvilinear fiber pathing

Crossref DOI link: https://doi.org/10.1007/s00158-026-04311-z

Published Online: 2026-06-06

Published Print: 2026-06

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

Authors

Namani Koureh, Sevda

Shahverdi, Hossein

Kakhsaz Malayeri, Nima

Amoozgar, Mohammadreza
License Information

Text and Data Mining valid from 2026-06-01

Version of Record valid from 2026-06-01
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Article History

Received: 7 October 2025

Revised: 1 February 2026

Accepted: 11 March 2026

First Online: 6 June 2026

Declarations

:

: The authors declare that they have no conflict of interest.

: This article does not contain any studies with human participants or animals performed by any of the authors.

: Codes are uploaded as supplementary material.

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