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A new "Ultimate Collector's" model with 1,559 pieces was released in 2013. In 2019, the Lego Group's annual Christmas gift to employees was a 1,038-piece Christmas X-wing, which also included Yoda's igloo and a sleigh. [36] In addition to the original T-65 X-wing, Lego has released several models of the newer T-70 X-wing.
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]
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 ]
Star Wars: X-Wing Second Edition is the second edition of the miniature war game designed by Jay Little and produced by Fantasy Flight Games that was first announced on May 1, 2018, with the first release on September 13 of the same year. On November 16, 2020, Atomic Mass Games (another subsidiary of Asmodee) announced that it would be ...
A lifting body is a foil or a complete foil-bearing body such as a fixed-wing aircraft. C L is a function of the angle of the body to the flow, its Reynolds number and its Mach number. The lift coefficient c l refers to the dynamic lift characteristics of a two-dimensional foil section, with the reference area replaced by the foil chord. [137 ...
The Y-wing assault starfighter/bomber are depicted as the primary fighter-bombers of the Galactic Republic, Rebel Alliance(stripped-down and heavily modified version of the former Galactic Republic Y-Wing), New Republic, and the newer Y-Wing model for the Resistance; being ideally suited for anti-shipping, close air support, and ground attack ...
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Camber is a complex property that can be more fully characterized by an airfoil's camber line, the curve Z(x) that is halfway between the upper and lower surfaces, and thickness function T(x), which describes the thickness of the airfoils at any given point. The upper and lower surfaces can be defined as follows: