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The Schneider Grunau 7 Moazagotl was a high-performance sailplane designed in Germany in 1933 specifically for fast, long distance flying using strong thermals. In 1937 it came second in the first World Gliding Championships, having previously made a flight of . ==Design and Development== Wolf Hirth was one of the first pilots to understand the glider characteristics necessary for cross-country flying on days with separated, strong thermals. It had to be equipped with a ballast tank to fly fast between thermals and be stable and efficient in the continuous, lift-gaining circling within the thermals, calling for high-aspect ratio wings with dihedral. He commissioned Edmund Schneider to build a one-off example, to be designed by Friedrich Wenk.〔 The result was the Moazagotl. Moazagotl was the nickname of Motz Gottlieb, formed from a corruption of his name, who was a farmer in the Silesian countryside near the Schneider works. He had noticed that with the wind in a particular direction, cloud formed over a nearby valley remained stationary even though the wind was strong. The phenomenon was communicated to meteorologists at an observatory near Breslau and their director passed on the observations to the glider pilots at Grunau, who thus became the first to exploit wave lift.〔〔 The Moazagottl was a high gull wing glider. The inner third of the span carried a dihedral of about 8° and was rectangular in plan. Single, broad-chord faired lift struts on each side braced these sections from about 20% of the span to the lower fuselage. Outboard the wing had no dihedral and was strongly swept on the leading edge, resulting in marked taper. Long ailerons occupied the whole trailing edge of each outer panels; these were slightly tapered and projected behind the trailing edge of the inner sections. The wing was built around a single, swept main spar which was straight in plan, simplifying its change in direction between the inner and outer panels. Diagonal sub-spars ran inwards and rearwards from it between the lift strut attachment points and the fuselage. Plywood skinning forward of these spars around the leading edge formed a D-box; aft, the wing, including the aileron, was fabric covered.〔 Its fuselage was ply covered and roughly oval in cross section, with a somewhat pointed nose and tapering gently and uniformly from wing to tail. The cockpit, just ahead of the leading edge, was enclosed by a plywood cover in Musterle fashion, providing illumination and limited views through small windows and portholes. Instrumentation was generous, including a variometer though lacking an artificial horizon for cloud flying. of water ballast was contained in a tank behind the pilot's seat. At the rear a tapered all moving tailplane was mounted just above the fuselage and far enough forward to need only a small cut out for rudder movement. All tail surfaces were largely fabric covered, with ply leading edges. There was no fin but the balanced rudder was much increased in chord and area after early flight tests demonstrated the power of the ailerons. The Moazagotl landed on a slender skid that reached from nose to mid chord, assisted by a faired tail skid.〔 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Schneider Moazagotl」の詳細全文を読む スポンサード リンク
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