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Akaflieg Darmstadt D-28 Windspiel
・ Akaflieg Darmstadt D-29
・ Akaflieg Darmstadt D-30 Cirrus
・ Akaflieg Darmstadt D-34
・ Akaflieg Darmstadt D-36 Circe
・ Akaflieg Darmstadt D-38
・ Akaflieg Darmstadt D-39
・ Akaflieg Darmstadt D-40
・ Akaflieg Darmstadt D-41
・ Akaflieg Darmstadt D-6 Geheimrat
・ Akaflieg Darmstadt D-7 Margarete
・ Akaflieg Darmstadt D-9 Konsul
・ Akaflieg Darmstadt/Akaflieg München DM1
・ Akaflieg Karlsruhe
・ Akaflieg Köln LS11


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Akaflieg Darmstadt D-28 Windspiel : ウィキペディア英語版
Akaflieg Darmstadt D-28 Windspiel

The Akaflieg Darmstadt D-28 Windspiel ((英語:Greyhound)) was a single-seat, high-performance sailplane designed in Germany in the early 1930s. Intended to exploit a growing understanding of thermal soaring, it was small and manoeuvrable, with a 12 m span; silk-covered for lightness, it weighed less (empty) than its pilots. It held the world straight-line distance record for a time in 1934.
==Design and development==

The Akademische Fliegergruppe of the Technical University of Darmstadt was first formed in 1921. It was, and is, a group of aeronautical students who design and construct aircraft as part of their studies and with the help and encouragement of their university. They began with gliders optimised for hill soaring with long span, high aspect ratio wings. By the early 1930s, partly through the experiences of the Darmstadt Musterle in the USA, there was a better understanding of "blue" thermals and the Darmstadt group sought to exploit these small, weak currents with a light, manoeuvrable aircraft that could stay within their rising columns. The result was the D-28 Windspiel, combining a 12 m (39 ft 4 in) span with the lowest weight achievable with the plywood and fabric materials of the time.〔〔
The D-28 was a wood-framed aircraft with a high, cantilever, single-spar wing, Akaflieg's established layout. It utilised the high-lift-to-drag ratio Göttingen 535 profile that Akaflieg had used on the Konsul and Darmstadt, though thinned by 10% to reduce drag. The structure also followed Akaflieg's previous use of wooden frames and stress-bearing plywood skin on the fuselage and leading edges of flying surfaces, with fabric covering elsewhere, but with greater attention to precision, the removal of unneeded material and metering of adhesives. The wing leading edge ply was only 1 mm (0.039 in) thick, and the fuselage was constructed without longerons. Instead of the standard aircraft linen, for lightness the Windspiel was covered in silk. The empty weight of the completed Windspiel was 55.5 kg (112 lb), a good deal less than that of most of its pilots.〔
In plan, the wing was straight-tapered with elliptical tips. The whole of the trailing edge was occupied by camber-changing flaperons, attached to selected ribs rather than to a subsidiary spar as usual, another weight-saving measure. The hinge gap was sealed with 500 μm (0.02 in) ply strips. The wing was mounted, as with several earlier Akaflieg sailplane, on a narrow, faired pylon, with the cockpit in front of it and under the leading edge. The upper fuselage from the nose to the front of the pylon was detachable in a single piece, together with the cellophane single curvature glazing, so the pilot could access the cockpit. The Windspiel's fuselage was slender and oval in cross section, with a short skid under the centre section and small tail bumper as an undercarriage. The horizontal tail was straight-tapered, with the tailplane fixed to the top of the fuselage and carrying elevators with a central cut-out for rudder movement. The tall, straight-edged rudder was an all-moving one, but of an unusual design, divided vertically into two sections, with the front part carrying the rear surface. When the front surface moved, the larger-area, deeper rear surface further deflected by the same amount again, presenting a cambered surface. As on the Konsul, the rudder and ailerons were interconnected to ease yaw correction in turns.〔
The date of the first flight is uncertain, but building was planned to start over the winter of 1931–32,〔 and the Windspiel was performing record flights by early 1934.〔 As its careful construction was slow, taking some 7,000 hours,〔 a 1933 date is plausible. In flight it achieved the tight turns required to stay within small thermals; a medium-level turn with a bank angle of 25° produced an 80 m (260 ft) radius circle.〔
After its 1935 accident and rebuild, the Windspiel was a little heavier, but the only major alteration was the separation of the full-span flaperons into inboard flaps and outboard ailerons.〔

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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