Aircraft
A technology for aircraft and thrusters, applied in the field of aircraft, can solve problems such as inability to provide structural efficiency
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[0031] refer to figure 2 A first aircraft 40 is shown. The aircraft includes a fuselage 42 ; a pair of wings 44 extending generally perpendicular to and extending from the fuselage 42 ; and an empennage located aft of the fuselage 42 . The tailplane comprises vertical and horizontal tailplanes 60 , 66 .
[0032] Wingspan is defined by the distance between wingtips 49 . Each airfoil 44 includes a leading edge 45 and a trailing edge 47 which together define a chord extending therebetween. The ratio of the wingspan to the chord length defines the aspect ratio. as from figure 2 As can be seen, the chord length varies along the span, from a relatively large chord length at the root adjacent to the fuselage 42 to a relatively small length at the wing tip 49 . With the chord varying along the span like this, the aspect ratio AR can be defined as the square of the span b divided by the area S of the wing plane:
[0033]
[0034] Although higher aspect ratios such as up to 3...
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