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後退・前進翼型結合翼機の低速風洞試験
後退・前進翼型結合翼機の低速風洞試験
Digital
文書・図像類
藤枝, 郭俊, 伊藤, 婦美子, 岩崎, 昭人, 藤田, 敏美, 滝澤, 直人, Fujieda, Hirotoshi, Ito, Fumiko, Iwasaki, Akihito, Fujita, Toshimi, Takizawa, Naoto
航空宇宙技術研究所
1996-07
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
695
p.1-19
Other Libraries in Japan
Subject Heading
結合翼機 後退翼 前進翼 水平尾翼 六分力測定
翼端剥離
低速風洞試験 可視化試験 揚抗比 joined wing ...
Note (General)
...施した。さらに後退角付き主翼の
翼端剥離
を遅らせるために、主翼前縁下面...
...丸棒を利用した簡易な整形により
翼端剥離
が約5度遅くなり、最大揚力が増大し、揚抗比および機体全体の空...
Reached to the end of result.
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