Aircraft aerofoil

B - Operations – Transporting – 64 – C

Patent

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244/34

B64C 3/00 (2006.01) B64C 3/14 (2006.01)

Patent

CA 1052358

ABSTRACT OF THE DISCLOSURE A supercritical aerofoil having a large leading edge radius of curvature, a radius of curvature over substantially the whole upper surface appreciably higher than the mean radius over the front half of the lower surface, a concave surface to the rear half of the lower surface, and a thickness/chord ratio of 10 - 14%.

247071

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