Aircraft having improved strake configuration

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 45A, 244130, B64C 126, B64C 2306

Patent

active

043789226

ABSTRACT:
An aircraft has a series of strakes in the form of laterally projecting bs (low aspect ratio semi-delta type aerofoils) extending longitudinally rearwards from and on each side of the nose, each barb lying substantially parallel to the longitudinal axis.

REFERENCES:
patent: 2694357 (1954-11-01), Lee
patent: 3333794 (1967-08-01), Lewis
patent: 3744745 (1973-07-01), Kerker et al.
patent: 4176813 (1979-12-01), Headley et al.
patent: 4225102 (1980-09-01), Frosch et al.

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