タイトル | Effects of Systematic Changes of Trailing-edge Angle and Leading-edge Radius on the Variation with Mach Number of the Aerodynamic Characteristics of a 10-percent-chord-thick NACA Airfoil Section |
本文(外部サイト) | http://hdl.handle.net/2060/19930085943 |
著者(英) | Summers, James L; Graham, Donald J |
著者所属(英) | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
発行日 | 1949-09-26 |
言語 | eng |
内容記述 | |
レポートNO | 93R15233 NACA-RM-A9G18 |
権利 | No Copyright |
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