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The Akaflieg Darmstadt D-17 Darmstadt, also called the Darmstadt D-17 and Darmstadt I, was a high performance, single seat, cantilever monoplane sailplane, designed and built by a German University student design group in 1927. It was followed in 1928 by the Akaflieg Darmstadt D-19 Darmstadt 2, a similar aircraft with a new profile, longer span wing. ==Development== The Akademische Fliergruppe 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. By 1927 the group were producing a range of designs traceable back to their 1923 Konsul and some of these were professionally built outside the University. The D-17, originally known simply as the Darmstadt and later as the Darmstadt 1, was one such.〔 The D-17 was a wood framed aircraft with a high, cantilever, single spar wing with stressed plywood covering from the spar to the leading edge and fabric covered aft. Its 16 m (52 ft 6 in) was built in three parts, a 6 m (19 ft 9 in) inner section with constant chord and thickness and outer panels which tapered in both chord and thickness to elliptical tips. The D-17 had the thick, high lift to drag ratio Göttingen 535 profile that Akaflieg had first used on the Konsul. Ailerons mounted on slightly angled hinges occupied the whole trailing edges of the outer panels. No flaps, airbrakes or spoilers were fitted, normal for the time.〔 The fuselage of the Darmstadt was a plywood skinned, oval cross sectioned semi-monocoque, slightly tapered and more rounded towards the tail. The open, unscreened cockpit was placed immediately ahead of the wing leading edge with the pilot's head against the front of a low, long chord, faired pylon which supported the wing. A short undercarriage skid was attached to the fuselage underside, aided by a small tailskid. The D-17 had all moving tail surfaces with straight edges, rounded tips and tapered by forward sweep on their trailing edges. The large rudder extended to the keel, moving in a cut-out in the one piece elevator.〔 In 1928 a close relative of the D-17, the D-19 Darmstadt 2, was flown.〔 Designed by F. Gross,〔 the main difference between it and the D-17 was the wing which had a 2 m (6 ft 7 in) greater span, making the D-19 an 18 m (59 ft 1 in) sailplane. The central panel span was increased to 7.62 m (25 ft). The D-19's wing area was only slightly higher, with the result that the aspect ratio was increased from 15.4 to 19.4. The D-19 used an more symmetric Joukowsky profile in place of the strongly cambered Göttingen 535, so decreasing the pitching moment; over the outer panels the thickness/chord ratio reduced continuously from 15% to 8. There were also smaller refinements around the cockpit and pylon and a deeper, less rounded fuselage profile.〔 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「Akaflieg Darmstadt D-17 Darmstadt」の詳細全文を読む スポンサード リンク
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