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| 报告编号 | NACA-WR-A-65 |
| 来源ID | NTRS_Document_ID: 19930092690 |
| Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel | |
| Erickson, Albert L | |
| 英文摘要 | A pursuit type airplane encountered severe diving moments in high-speed dives which make recovery difficult. For the purpose of investigating these diving moments and finding means for their reduction, a 1/6-scale model of the airplane was tested in the 16-foot high-speed wind tunnel at Ames Aeronautical Laboratory. The test results indicate that up to a Mach number of at least 0.75, the limit of the tests, the dive-recovery difficulties can be alleviated and the longitudinal maneuverability improved by the substitution of a long symmetrical fuselage for the standard fuselage. |
| 英文关键词 | SUBSONIC SPEED FUSELAGES AIRCRAFT MODELS MANEUVERABILITY FLIGHT CONTROL AIRCRAFT MANEUVERS MACH NUMBER SCALE MODELS TRANSONIC WIND TUNNELS |
| 出版年 | 1942 |
| 报告类型 | Technical Report |
| 语种 | 英语 |
| 国家 | 美国 |
| URL | http://hdl.handle.net/2060/19930092690 |
| 资源类型 | 科技报告 |
| 条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/258273 |
| 推荐引用方式 GB/T 7714 | Erickson, Albert L. Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel,1942. |
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