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Publikováno v:
Aerospace, Vol 8, Iss 11, p 334 (2021)
This article presents a modal correlation and update carried out on an aeroelastic wind tunnel demonstrator representing a conventional passenger transport aircraft. The aim of this work is the setup of a corresponding numerical model that is able to
Externí odkaz:
https://doaj.org/article/9244582d4663406a86dfd8973526484b