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・ Albatros C.VIII N
・ Albatros C.X
・ Albatros C.XII
・ Albatros C.XIII
・ Albatros C.XIV
・ Albatros C.XV
・ Albatros D.I
・ Albatros D.II
・ Albatros D.III
・ Albatros D.IV
・ Albatros D.IX
・ Albatros D.V
・ Albatros D.VI
・ Albatros D.VII
・ Albatros D.X
Albatros D.XI
・ Albatros D.XII
・ Albatros Dr.I
・ Albatros Dr.II
・ Albatros Flugzeugwerke
・ Albatros G.I
・ Albatros G.II
・ Albatros G.III
・ Albatros J.I
・ Albatros J.II
・ Albatros L 100
・ Albatros L 35
・ Albatros L 45
・ Albatros L 58
・ Albatros L 59


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Albatros D.XI : ウィキペディア英語版
Albatros D.XI
__NOTOC__

The Albatros D.XI was a German single-seat fighter biplane first flown in February 1918. It was the first Albatros design to use a rotary engine, in the form of the 120 kW (160 hp) Siemens-Halske Sh.III, and also featured a new wing construction with diagonal struts from the fuselage replacing traditional wire bracing.
==Design & development==
The wings had unequal spans with the upper planes having greater span than the lower ones, and were braced by I-struts with an aerofoil cross-section, additional rigidity being provided by twinned diagonal struts from the base of these to the top of the fuselage, located where the "landing wires" of a normal wire-braced biplane would be. The use of a rotary engine necessitated a large-diameter propeller and a correspondingly tall undercarriage.
The D.XI was armed with the same twin 7.92 mm (.312 in) Spandau LMG 08/15 machine guns employed on other Albatros fighters. Two prototypes were built, the first having balanced, parallel-chord ailerons and a four-blade propeller; and the second with inversely tapered, unbalanced ailerons and a two-blade propeller. The D.XI was not put into production.

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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