The strake (102) has a leading edge (110).
The lift device (100) further comprises a leading-edge flap (112) coupled to the strake leading edge (110).
A fin having a leading edge, a trailing edge opposing the leading edge, and a plurality of leading holes substantially centered along a leading axis.
The leading edge rib (472) is configured to form a leading edge chamber (463) in conjunction with the leading edge (446) of the skin (460).
Each aerofoil has pressure side, a suction side, a leading edge region and a leading edge foot extending from the leading edge region, the leading edge foot has a ridge line.
The blade may have a leading edge and a sheath may extend along the leading edge of the blade.
The blade includes a leading edge and a trailing edge.
The airfoil has a trailing edge extending to a leading edge.
Conductive straps are provided along the leading edge of the opening and have widths sufficient to cover a substantial majority of the leading edge to form a shielded interface along the leading edge.
The invention relates to a structure of a leading edge (1), in particular for the air intake of an aircraft nacelle, including a leading edge (2) and an inner partition wall (3) defining a longitudinal compartment (5) inside the leading edge (2).
The upper surface has a leading edge (2a) and a trailing edge (2b).
bonnet leading edge reference line
The concave leading edge (24) is provided with a coextensive protrusion (26) and the convex leading edge is provided with a coextensive recess (27).
The control wing (7) has a leading edge (11) and is angled laterally downwardly toward the leading edge (11).
Each fan blade has a leading edge.
leading edge junction fairing
The invention relates to a wing comprising a wing leading edge (1), a wing trailing edge (2), and a wing border (3) running between the wing leading edge (1) and the wing trailing edge (2) on the free end.
Each barb is defined by a leading edge and a trailing edge.
The first implant component has a leading edge and a trailing edge.
A leading edge for use as a leading edge reinforcement on a blade or air foil part.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Traduction Translation Traducción Übersetzung Tradução Traduzione Traducere Vertaling Tłumaczenie Mετάφραση Oversættelse Översättning Käännös Aistriúchán Traduzzjoni Prevajanje Vertimas Tõlge Preklad Fordítás Tulkojumi Превод Překlad Prijevod 翻訳 번역 翻译 Перевод