Manoeuverable supercritical wing section

Details Manoeuverable supercritical wing section Manoeuverable supercritical wing section

1984-07-20

1988-01-12

Walsh, Donald P.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244 35A, B64C 314

Patent

active

047186194

ABSTRACT:
The manoeuverable supercritical wing section with a t/c ratio of 8-9%, flexible at 70%-80% chord by means of a flap to induce expansion thereover, and perhaps having a minimum curvature region on the upper surface just ahead of the flexing region.

REFERENCES:
patent: 3309042 (1967-03-01), Edwards
patent: 4072282 (1978-02-01), Fulker
patent: 4361299 (1982-11-01), Sharrock

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