著者

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

出版者

一般社団法人 日本航空宇宙学会

雑誌

日本航空学会誌 (ISSN:00214663)

巻号頁・発行日

vol.2, no.10, pp.255-263, 1954-10-31 (Released:2009-07-09)

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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.