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Publikováno v:
Materials, Vol 17, Iss 11, p 2756 (2024)
Analytical modeling of the squeezing force for aircraft wings and fuselage panels in the existing literature usually assumes uniform deformation of the rivets, while in reality, the deformation of the rivets is non-uniform. To achieve high-quality sq
Externí odkaz:
https://doaj.org/article/881e74c4fec848c1a5890aa50bd9ffff