Nacelle and wing assembly

Aeronautics and astronautics – Aircraft structure – Details

Patent

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Details

244 55, 244 35R, B64D 2902

Patent

active

048156809

ABSTRACT:
A nacelle wing combination wherein said nacelle can be mounted below the wing and positioned closely to the wing, without creating excessive nacelle induced drag. The wing is contoured so that peak low pressures below the wing occur near the mid chordwise location at the lower surface of the wing. Thus, the channeling of air passing over the nacelle and under the leading edge of the wing does not create supersonic velocities which would create excessive drag.

REFERENCES:
patent: 4314681 (1982-02-01), Kutney
patent: 4524928 (1985-06-01), Schmidt et al.

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