著者

上山 和夫 安部 正 杉木 勝昌 岡 雄生

出版者

一般社団法人 日本航空宇宙学会

雑誌

日本航空宇宙学会誌 (ISSN:00214663)

巻号頁・発行日

vol.22, no.247, pp.405-408, 1974 (Released:2009-05-25)

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A unique device, named "dihedral effect adjusting fin" is introduced in the development of Mitsubishi twin-turboprop business plane, MU-2G. This device, a fin attached to the wing tip tank, causes a modification of interference effect of wing tip tank with the main wing, and facilitates the adjustment with assurance of dihedral effect of an airplane with wing tip tank.In this note, the idea of dihedral effect adjusting fin and its application to the development of MU-2G plane are reviewed.