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X-wings with their s-foils locked in attack position as they assault the Death Star in Star Wars (1997 Special Edition) The T-65B X-wing was produced by the Incom Corporation, which had previously supplied the ARC-170 and Z-95 Headhunter starfighters to the Galactic Republic during the Clone Wars. When the Galactic Empire ordered them to ...
It would also serve as the in-universe inspiration for Incom's next starfighter, the X-wing. Like the X-wing, the ARC-170 features S-foils, which open during combat to shed waste heat, enlarge the starfighter's deflector shields, and function as stabilizer surfaces during atmospheric flight. [27] [29]
Clark Y is the name of a particular airfoil profile, widely used in general purpose aircraft designs, and much studied in aerodynamics over the years. The profile was designed in 1922 by Virginius E. Clark using thickness distribution of the German-developed Goettingen 398 airfoil. [1]
A foil generates lift primarily because of its shape and angle of attack. When oriented at a suitable angle, the foil deflects the oncoming fluid, resulting in a force on the foil in the direction opposite to the deflection. This force can be resolved into two components: lift and drag. This "turning" of the fluid in the vicinity of the foil ...
Star Wars: X-Wing is a miniature war game designed by Jay Little and produced by Fantasy Flight Games that was released at Gen Con during August 17, 2012. [2] [3] It features tactical ship-to-ship dogfighting between various types of starfighters set in the fictional Star Wars universe. [4]
Hydrofoiling wingsail catamaran 17. A sailing hydrofoil, hydrofoil sailboat, or hydrosail is a sailboat with wing-like foils mounted under the hull.As the craft increases its speed the hydrofoils lift the hull up and out of the water, greatly reducing wetted area, resulting in decreased drag and increased speed.
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Mean aerodynamic chord (MAC) is defined as: [6] = (), where y is the coordinate along the wing span and c is the chord at the coordinate y.Other terms are as for SMC. The MAC is a two-dimensional representation of the whole wing. The pressure distribution over the entire wing can be reduced to a single lift force
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