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・ LFC TV
・ LFCC
・ LFD
・ LFE
・ LFE (programming language)
・ LFER solvent coefficients (data page)
・ LFF
・ LFF Stadium
・ LFG
・ LFG Roland C.II
・ LFG Roland D.I
・ LFG Roland D.II
・ LFG Roland D.III
・ LFG Roland D.IV
・ LFG Roland D.IX
LFG Roland D.VI
・ LFG Roland D.VII
・ LFG Roland D.XV
・ LFG Roland D.XVI
・ LFG Roland D.XVII
・ LFG Roland G 1
・ LFG Roland Pfeilflieger
・ LFG V 101
・ LFG V 13
・ LFG V 20
・ LFG V 39
・ LFG V 40
・ LFG V 42
・ LFG V 52
・ LFG V 59


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LFG Roland D.VI : ウィキペディア英語版
LFG Roland D.VI

The Roland D.VI was a German fighter aircraft built at the end of World War I. It lost a fly-off to the Fokker D.VII, but production went ahead anyway as insurance against problems with the Fokker.
==Design and development==
The Roland D.VI was designed by the Luft-Fahrzeug-Gesellschaft (L.F.G.), (whose aircraft were made under the trade name "Roland" after 1914 to avoid confusion with the Luftverkehrsgesellschaft m.b.H (L.V.G.)) late in 1917, with the prototype being the 1000th aircraft to be built by L.F.G., first flying in November 1917.〔 The D.VI was a single bay biplane which discarded the L.F.G.-Roland patented ''Wickelrumpf'' (literally "wrapped body"), or semi-monocoque fuselage, constructed with two layers of thin plywood strips, diagonally wrapped around a male form to create a "half-shell", that used in previous L.F.G aircraft such as the Roland C.II, D.I and D.II in favour of the equally unusual (for aircraft use) ''Klinkerrumpf'' (or clinker-built) construction where the fuselage was built of overlapping thin strips of spruce over a light wooden framework.〔Gray and Thetford 1961, pp. 166–167.〕 Visibility for the pilot was good, while the aircraft had above average manoeuvrability.〔Gray and Thetford 1961, p. 167.〕

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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