Aircraft wing fence

Aeronautics and astronautics – Aircraft control – Vertical fins

Patent

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Details

114274, 244130, 244199, B64C 506

Patent

active

042380944

ABSTRACT:
An improved fluid fence which reduces drag on solid objects moving through a fluid environment and an airfoil or aircraft wing structure having an improved open fence on its surface improving the lift-to-drag characteristics of the airfoil.

REFERENCES:
patent: 1808996 (1931-06-01), Royster
patent: 2125738 (1938-08-01), Rose
patent: 2885161 (1959-05-01), Kerker et al.
patent: 3693913 (1972-09-01), Barland et al.
A. R. Weyl, "Stability of Tailless Aeroplanes", Aircraft Engineering, Apr. 1945, pp. 103-111.

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