AIRCRAFT COMPRISING A CENTRAL FAIRING THAT ADJUSTS THE PRESSURE ON THE WING STRUCTURES BY MEANS OF LOCAL GEOMETRIC DEFORMATIONS

An aircraft including: a fuselage and two wings to which engine nacelles are attached and that are each connected laterally to the fuselage, one on each side thereof, by a central fairing. The central fairing includes, facing each wing, two opposed surfaces connected one to a suction face side and t...

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Bibliographische Detailangaben
Hauptverfasser: JIMENEZ, PHILIPPE, NAMER, ARNAUD, FOL, THIERRY
Format: Patent
Sprache:eng ; fre ; ger
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