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The paper presents the design and analysis of a High Lift Two-Element Airfoil, RUKSAN-T20, for Medium Altitude Long Endurance (MALE) UAVs using CFD tools, specifically the MSES code. The design aims to achieve a maximum lift coefficient (CLmax) of 2.4 to enhance endurance performance, validated through wind tunnel testing at various Reynolds numbers. The results demonstrate significant improvements in aerodynamic characteristics compared to conventional single-element airfoils, confirming the feasibility of
- Author
- white flame
- Language
- EN