Oblique-wing supersonic aircraft

Details Oblique-wing supersonic aircraft Oblique-wing supersonic aircraft

1974-08-12

1976-07-27

Blix, Trygve M.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

B64C 340

Patent

active

039715353

ABSTRACT:
An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage. The pivotal attachments allow the airfoils to be yawed relative to the fuselage for high speed flight, and to be positioned at right angles with respect to the fuselage during take-off, landing, and low speed flight. The main wing and the horizontal stabilizer are upwardly curved from their center pivotal connections towards their ends to form curvilinear dihedrals.

REFERENCES:
patent: 3009670 (1961-11-01), Williams et al.
patent: 3028122 (1962-04-01), Riebe et al.
patent: 3047255 (1962-07-01), Wallis
patent: 3155344 (1964-11-01), Vogt
patent: 3454241 (1969-07-01), Riemerschmid
patent: 3455523 (1969-07-01), Mertel

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