| タイトル | An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel. Part III - Longitudinal-Control Characteristics TED No. NACA DE308 |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050019289 |
| 著者（英） | Kuhn, Richard E.; King, Thomas J., Jr. |
| 著者所属（英） | Bureau of Aeronautics (Navy); National Advisory Committee for Aeronautics. Langley Aeronautical Lab. |
| 発行日 | 1947-07-29 |
| 言語 | eng |
| 内容記述 | Tests have been conducted in the Langley high speed 7- by 10-foot tunnel over a Mach number range from 0.40 to 0.91 to determine the stability and control characteristics of an 0,08-scale model of the Chance Vought XF7U-1 airplane. The longitudinal-control characteristics of the complete model are presented in the present report with a limited analysis of the results. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | NACA-RM-L7H01-PT-3 |
| 権利 | No Copyright |
