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| 小型民用正常类飞机尾旋特性试飞技术研究 | |
| 引用本文： | 王启,张培田,冯瑞娜,李勤红,郑喜红.小型民用正常类飞机尾旋特性试飞技术研究[J].飞行力学,2006,24(3):66-69. |
| 作者姓名： | 王启 张培田 冯瑞娜 李勤红 郑喜红 |
| 作者单位： | 1. 西北工业大学航空学院,陕西,西安,710072 2. 中国飞行试验研究院飞机所,陕西,西安,710089 3. 中国飞行试验研究院,测试所,陕西,西安,710089 |
| 摘 要： | 简要介绍了按照CCAR-23部进行合格审定正常类飞机对尾旋试飞的要求,对小型民用飞机尾旋特性试飞方法进行了研究,结合具体型号进行了飞行试验验证,给出了该飞机的尾旋试飞结果。结果证明,该试飞技术适用于小型民用飞机型号合格审定尾旋试飞。 |
| 关 键 词： | 失速 尾旋 抗尾旋 |
| 文章编号： | 1002-0853(2006)03-0066-04 |
| 收稿时间： | 2005-06-09 |
| 修稿时间： | 2006-04-05 |
Flight Test Technology Research for Spin Characteristics for a Light Normal Category Civil Airplane |
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| WANG Qi,ZHANG Pei-tian,FENG Rui-na,LI Qin-hong,ZHENG Xi-hong.Flight Test Technology Research for Spin Characteristics for a Light Normal Category Civil Airplane[J].Flight Dynamics,2006,24(3):66-69. | |
| Authors: | WANG Qi ZHANG Pei-tian FENG Rui-na LI Qin-hong ZHENG Xi-hong |
| Abstract: | In this paper,the requirements of spin flight item for those normal category airplanes that certificated with part 23 of CCAR was introduced,the flight test technology of spin characteristics for a light civil airplane was investigated,and flight test validation was performed on the LE-500 airplane.At last the conclusion of the spin flight test was given.The result shows that this flight test technology is applicable to quotable for the certification of light civil airplanes. |
| Keywords: | stall spin antispin |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |