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Schempp-Hirth Göppingen Gö 4 : ウィキペディア英語版
Göppingen Gö 4

The Göppingen Gö 4 or Goevier is a German sailplane of the late 1930s used for training pilots. Its most notable features include side-by-side seating and dual controls, making the plane ideal for use as a trainer. It boasted average performance, compared to other gliders of the day, and was advertised as making the process of learning to fly sailplanes easier.
==Design and development==
The Goevier (or Gövier; Gö 4 read aloud in German) was designed as a modern trainer with side-by-side seating for easy communication between student and tutor, with performance comparable to that of the intermediate single seat trainers of the day such as the Grunau Baby and Göppingen Gö 1 Wolf. Its glide angle of 19:1 was rather better than that of both these aircraft (17:1).
It is a cantilever mid-wing monoplane. The wing has a single spar and a plywood covered D-box nose; aft of the spar the wing is fabric covered. The centre section is of constant chord and the outer panels tapered, with sweep on both edges. Here the trailing edge carries long span, broad chord ailerons with curved edges which extend aft of the centre section trailing edge, giving a roughly elliptical plan.
The side-by-side seat arrangement inevitably makes the front fuselage wider (945 mm; 37.4 in externally〔) than that of a single or tandem seat aircraft, though as the seats are just ahead of the main spar and the mid-wing placed at shoulder height, the interior opening into the wing roots provides extra working space. These roots were early examples of the use of plastics in gliders, formed from hessian soaked in phenolic resins and shaped in a mould.〔 The cockpit is enclosed with glazing and its roof line runs smoothly into that of the upper fuselage above the wing. The fuselage, plywood covered all over, tapers to the tail where the cross-section is shield shaped. The ply covered tailplane is mounted on a small step above the fuselage; together with the fabric covered elevators the horizontal tail is trapezoidal in plan with rounded tips.〔 The fin and rudder were altered several times during the development of the Goevier, initially with both broad and with the fin extending forward to the leading edge of the tailplane, but on all production models it is narrow and upright, carrying several slightly different rudder designs. From 1941 the rudder was aerodynamically balanced.〔〔 The Goevier lands on a monowheel undercarrige, with a skid reaching forward from it to the nose and with a small tail skid.〔
The Goevier V-1 made its first flight on 30 November 1937, piloted by Heinz Kensche.〔 Production began at Göppingen the following October.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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