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Fluid Coupled Structural Analysis and Optimization of Expanded Polystyrene-Fiber-Reinforced Composite Wing of an Unmanned Aerial Vehicle

Crossref DOI link: https://doi.org/10.1007/s11029-024-10185-3

Published Online: 2024-04-26

Published Print: 2024-05

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

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