Vortex reducing wing tip

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

B64C 2100

Patent

active

041084039

ABSTRACT:
An airfoil tip is constructed to droop downward and extend aft of the trailing edge of the air foil structure and to include air foil configuration both chordwise and spanwise with camber in both the chordwise and spanwise directions and further including a vortex opposing twist in the chordwise direction.

REFERENCES:
patent: 2123096 (1938-07-01), Charpentier
patent: 3411738 (1968-11-01), Sargent
patent: 3974986 (1976-08-01), Johnstone

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