Arab J Sci Eng
 2024
DOI: 10.1007/s13369-024-08837-6
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Design of a Novel Aerofoil of a Light Aircraft for Robust Aerodynamic Performance at High Reynolds Number Regime Using XFLR5

Farzana Akter,
Md. Araful Hoque,
Kazi Ahasan Ekram
et al.
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