Airfoil trailing edge

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/14 (2006.01)

Patent

CA 2354383

An aerofoil wing comprising upper and lower surfaces meeting at the leading and trailing edges and a camber line representing the curvature of the aerofoil comprising at least two regions of substantially linear increases in curvature and wherein the increases in curvature are of monotonically increasing magnitude. Preferably there are three regions of substantially linear increases in curvature.

Aile à profil aérodynamique qui comprend des surfaces supérieure et inférieure se rencontrant au niveau de bords d'attaque et de fuite, et une ligne de cambrure représentant la courbure de l'aile et comportant au moins deux zones d'augmentation pratiquement linéaire de la courbure, les augmentations de la courbure présentant une progression monotone. De préférence la courbure présente trois zones d'augmentation linéaire.

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