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).<ref name=SSUK>{{#invoke:citation/CS1|citation |CitationClass=web }}</ref><ref name="Brütting">Template:Cite book</ref>

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.<ref name=SimonsI>Template:Cite book</ref>

The side-by-side seat arrangement inevitably makes the front fuselage wider (945 mm; 37.4 in externally<ref name=SimonsI/>) 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.<ref name=SSUK/> 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.<ref name=SimonsI/> 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.<ref name=SSUK/><ref name=SimonsI/> The Goevier lands on a monowheel undercarriage, with a skid reaching forward from it to the nose and with a small tail skid.<ref name=SimonsI/>

The Goevier V-1 made its first flight on 30 November 1937, piloted by Heinz Kensche.<ref name=SSUK/> It was often towed by a Klemm Kl 25.Template:Sfn Production began at Göppingen the following October.<ref name=SimonsI/>

Operational history

In a flight covering 1–3 June 1939, Josef Füringer and Hofmann flew a Goevier to a new world duration record of 49 h 45 min.<ref name="Brütting"/>

A Goevier was used to develop the now ubiquitous Schempp-Hirth airbrake with its parallel ruler action.<ref name=SimonsI/>

During World War II the Goevier was the standard advanced trainer with both the National Socialist Flyers Corps and the Werrmacht Luft gliding units.<ref name=SSUK/>

Goeviers have been regular attendees at Veteran Glider meetings in the later part of the last century.<ref name=VGC>Template:Cite journal</ref> In 2010 one Goevier II and four Goevier IIIs remained on the civil registers of European countries, three in Germany and two in the Netherlands.<ref name=EuReg>Template:Cite book</ref>

Variants

Data from The Göppingen Gö 4 (GOEVIER),<ref name=SSUK/> Der berühmtesten Segelfluzeuge,<ref name="Brütting"/> and Sailplanes 1920-1945<ref name=SimonsI/>

Goevier I

Prototype V-1. Length 6.74 m (22 ft 1 in), span 14.80 m (48 ft 6.7 in). Broad fin and rudder.

Goevier II

Production model before and during World War II. About 100, possibly more, built before February 1941. Another 6 were built by Fokker immediately post-war.<ref name=VGC/> Length 7.26 m (23 ft 10 in), span 14.73 m (48 ft 4 in). Narrower fin and rudder. From 1941 with horn-balanced and slightly less rounded rudder on same fin.

Goevier III

(aka Hirth-Hütter Goevier III) – Dipl.-Ing. Wolf Hirth/Wolfgang Hütter.Post-war production model, prototype V-2. About 20 built. As later Goevier II but length 6.24 m (20 ft 5.6 in).

Hirth Hi-20 MoSe

Powered, self launching version completed in 1941. Retractable propeller.

Aircraft on display

Of the several surviving airframes, the following are on public static display.<ref name=Ogden>Template:Cite book</ref>

• Goevier II: OE-0104, Aviaticum Wiener Neustadt, Austria
• Goevier III: D-6007, Deutsches Museum - Flugwerft Schleissheim, Oberschleissheim, Germany
• Goevier III: D-1084, Deutsches Segelflugmuseum mit Modellflug, Wasserkuppe, Germany

References

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