Lift and twist control using trailing edge control surfaces...

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Reexamination Certificate

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07004428

ABSTRACT:
An aircraft includes a fuselage, thin supersonic wings on the fuselage, there being trailing edge flaps carried by the wings, the flaps configured to provide flap deflection to simultaneously control wing twist and to reduce drag, when the aircraft is operated at subsonic flight conditions.

REFERENCES:
patent: 3188022 (1965-06-01), Torsten
patent: 3204895 (1965-09-01), Razak
patent: 3870253 (1975-03-01), Leirdy et al.
patent: 4146200 (1979-03-01), Borzachillo
patent: 4165058 (1979-08-01), Whitener
patent: 4180224 (1979-12-01), Ryle, Jr.
patent: 4725020 (1988-02-01), Whitener
patent: 5082207 (1992-01-01), Tulinius
patent: 5088661 (1992-02-01), Whitener
patent: 5518204 (1996-05-01), Tracy
patent: 5740991 (1998-04-01), Gleine et al.
patent: 5875998 (1999-03-01), Gleine et al.
patent: 5897076 (1999-04-01), Tracy
patent: 5984229 (1999-11-01), Hollowell et al.

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