| タイトル | Investigation of the aerodynamic characteristics in pitch and sideslip of a 45 degree swept-wing airplane configuration with various vertical locations of the wing and horizontal tail : static lateral and directional stability; Mach numbers of 1.41 a |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930089962 |
| 著者（英） | Robinson, Ross B; Spearman, M Leroy |
| 著者所属（英） | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
| 発行日 | 1957-12-27 |
| 言語 | eng |
| 内容記述 | |
| レポートNO | 93R19252
NACA-RM-L57J25a |
| 権利 | No Copyright |
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