AIRCRAFT PORTION WITH REDUCED WAVE DRAG

An aircraft portion includes a fuselage oriented in a longitudinal direction, an airfoil made up of at least one pair of wings arranged on either side of the fuselage in a transverse direction orthogonal to the longitudinal direction, and an airfoil-fuselage junction fairing at the interface between...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LOYATHO, Ximun, JOHAN, Zdenek, MERLET, Aurélien, ROGE, Gilbert
Format: Patent
Sprache:eng
Schlagworte:
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