| タイトル | Flight Studies of the Horizontal-Tail Loads Experienced by a Fighter Airplane in Abrupt Maneuvers |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050241737 |
| 著者所属（英） | National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
| 発行日 | 1944-01-01
1944 |
| 言語 | eng |
| 内容記述 | Field measurements were made on a fighter airplane to determine the approximate magnitude of the horizontal tail loads in accelerated flight. In these flight measurements, pressures at a few points were used as an index of the tail loads by correlating these pressures with complete pressure-distribution data obtained in the NACA full-scale tunnel. In addition, strain gages and motion pictures of tail deflections were used to explore the general nature and order of magnitude of fluctuating tail loads in accelerated stalls. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | NACA/TR-792 |
| 権利 | No Copyright |
