Wing tip airfoils

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 91, B64C 508

Patent

active

045951608

ABSTRACT:
The subject invention relates to a new and improved airfoil design. More particularly, an airfoil design is disclosed which improves efficiency by taking advantage of the vortex created at the wing tips.

REFERENCES:
patent: 1112126 (1914-09-01), Emmons
patent: 2576981 (1951-12-01), Vogt
patent: 2743888 (1956-05-01), Lippisch
patent: 3270988 (1966-09-01), Cone, Jr.
patent: 3712564 (1973-01-01), Rethorst
patent: 3997132 (1976-12-01), Erwin
patent: 4108403 (1978-08-01), Finch
patent: 4172574 (1979-10-01), Spillman
patent: 4190219 (1980-02-01), Hackett
patent: 4272043 (1981-06-01), Spillman
patent: 4377267 (1983-03-01), Haworth
Jordan, "Development of Test Methods for Scale Model Simulation . . . ", NASA Langley Res. Conf., 1980, Gulfstreamer, vol. 5, No. 6, Winter 1976.

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