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

    Design of a Novel Aerofoil of a Light Aircraft for Robust Aerodynamic Performance at High Reynolds Number Regime Using XFLR5 von Akter, Farzana, Hoque, Md. Araful, Ekram, Kazi Ahasan, Saha, Badhan, Hasan, Md. Jahid


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