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Design of a Novel Aerofoil of a Light Aircraft for Robust Aerodynamic Performance at High Reynolds Number Regime Using XFLR5

Crossref DOI link: https://doi.org/10.1007/s13369-024-08837-6

Published Online: 2024-02-26

Published Print: 2024-08

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

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