Wing-sections, in particular aircraft lift-wing sections

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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B64C 314

Patent

active

045249288

ABSTRACT:
A wing-section design for lift-wings, for instance for fighter aircraft, where the section design specifically depends on specially designed top and bottom sides of the section and where the top side curvature along the depth of section depends only upon the operational Mach number, while the bottom side curvature additionally depends on the section thickness and the desired lift range.

REFERENCES:
patent: 4121787 (1978-10-01), Wilby
patent: 4413796 (1983-11-01), Bousquet

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