Laminar flow wing for transonic cruise

Details Laminar flow wing for transonic cruise Laminar flow wing for transonic cruise

B - Operations, Transporting

64

C

B64C 3/10 (2006.01) B64C 1/00 (2006.01) B64C 3/14 (2006.01) B64C 21/00 (2006.01)

Patent

CA 2503270

In combination, an aircraft wing and fuselage, comprising the wing having camber at or near the wing leading edge which has blunted sharpness and low sweep angle, and the fuselage having indentation along the wing side thereof, and lengthwise of the fuselage.

L'invention concerne une combinaison une aile et un fuselage d'avion combinés. L'aile présente une cambrure au niveau ou à proximité du bord d'attaque de l'aile, lequel est obtus et possède un angle de flèche bas, et le fuselage présente une indentation le long de son coté aile et dans le sens longitudinal du fuselage.

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