タイトル | Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections |
本文(外部サイト) | http://hdl.handle.net/2060/19930086147 |
著者(英) | Berggren, Robert E; Graham, Donald J |
著者所属(英) | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
発行日 | 1950-07-03 |
言語 | eng |
内容記述 | |
レポートNO | 93R15437 NACA-RM-A50D04 |
権利 | No Copyright |
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