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: Fol, Thierry, Jimenez, Philippe, Namer, Arnaud
Format: Patent
Sprache:eng
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