Highly swept canard with low sweep wing supersonic aircraft...

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Reexamination Certificate

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06857599

ABSTRACT:
An aircraft, comprising a fuselage having an elongated, narrow forward portion, a main wing carried by a rear portion of the fuselage, a canard wing carried by said fuselage forward portion and having swept back leading and trailing edges tapering toward a tip or tips, the canard wing having less lifting surface than the main wing.

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patent: 5740984 (1998-04-01), Morgenstern
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patent: 5992796 (1999-11-01), Smith
patent: D453014 (2002-01-01), Fraser
patent: 6575406 (2003-06-01), Nelson
patent: 6705567 (2004-03-01), Dong et al.

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