タイトル | Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at Mach numbers form 0.75 to 1.96 |
本文(外部サイト) | http://hdl.handle.net/2060/19930089308 |
著者(英) | Guy, Lawrence D; Brown, Hoyt V |
著者所属(英) | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
発行日 | 1955-02-15 |
言語 | eng |
内容記述 | |
レポートNO | 93R18598 NACA-RM-L54K16a |
権利 | No Copyright |
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