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M. Sivapragasam

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Aug 2026

Low-Reynolds-Number Aerodynamics of Airfoils with Sharp Leading Edges

The aerodynamic performance of conventional (rounded leading-edge) and reversed (sharp leading-edge) airfoils is investigated in the low Reynolds number regime. Computations are performed in the range Re ∈ [1x108, 8x104]. The results show significant differences in the flow structures and the aerodynamic characteristic...

T. Grishma, Kavya Nagaraj, M. Sivapragasam · 0 citations

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