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・ Junkers Ju 86
・ Junkers Ju 87
・ Junkers Ju 88
・ Junkers Ju 89
・ Junkers Ju 90
・ Junkers Jumo 004
・ Junkers Jumo 204
・ Junkers Jumo 205
・ Junkers Jumo 210
・ Junkers Jumo 211
・ Junkers Jumo 213
・ Junkers Jumo 222
・ Junkers Jumo 223
・ Junkers K 16
・ Junkers K 37
Junkers K 47
・ Junkers L1
・ Junkers L2
・ Junkers L5
・ Junkers L55
・ Junkers L88
・ Junkers Profly
・ Junkers Profly Junkers Trike
・ Junkers Profly Ultima
・ Junkers T 19
・ Junkers T 23
・ Junkers T.21
・ Junkers W 33
・ Junkers W 34
・ Junkersdorf


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Junkers K 47 : ウィキペディア英語版
Junkers K 47

The Junkers K 47 was a fighter developed in Sweden by the Swedish subsidiary of the German firm Junkers during the late 1920s, a civil development of which was designated the A 48.
==Design and development==
Designed to meet a requirement of the Turkish government for a new fighter, the K 47 was a strut-braced, low-wing monoplane of conventional design. Two open cockpits accommodated the pilot and tail-gunner, and the empennage was designed with twin vertical surfaces to maximise the rearward field of fire. The main units of the fixed, tailskid undercarriage shared part of the truss structure that braced the wings. The design was originally undertaken by Karl Plauth, but completed after his death by Hermann Pohlmann. The aircraft had to be built at first in Sweden, because it was patently a military-type aircraft and therefore banned in Germany according to the terms of the Versailles Treaty.

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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