日本航空学会誌
Online ISSN : 2432-3039
Print ISSN : 0021-4663
東洋航空工業株式会社製FD-25A機体強度試験について1)
疋田 遼太郎武田 峻市川 輝雄田辺 哲夫馬場 敏治檜山 斉雄得能 健次郎
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ジャーナル フリー

1954 年 2 巻 10 号 p. 255-263

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抄録
The aircraft Model FD-25 A is a trainer manufactured by the TOYO-KOKU-KOGYO Ltd., with the design of the Fletcher Aircraft Corp. To demonstrate the strength of this aircraft, the load was applied under a system of forces simulating as closely as possible those required in the regulation of C.A.A. of Japan. In this paper, the result of tests, the method of load calculation and the loading apparatus were reported and discussed.
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© The Japan Society for Aeronautical and Space Sciences
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