| 直升机由悬停过渡到前飞的飞行特性研究 |
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| 引用本文： | 熊良玉,向锦武.直升机由悬停过渡到前飞的飞行特性研究[J].航空学报,1999,20(5):455-457. |
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| 作者姓名： | 熊良玉 向锦武 |
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| 作者单位： | 北京航空航天大学,飞机设计研究所,北京,100083 |
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| 摘 要： | 研究了直升机由悬停转前飞的过渡飞行中高度和速度变化。首先研究了计算方法，并以 Ｓ Ａ３６５ Ｎ 型直升机为例进行了核算比较，验证了分析方法的可行性和合理性；最后对一般直升机在各种发动机故障状态及操纵输入进行了分析计算， 得出了一些有意义的结论，这些结论将为今后的实际飞行提供有益的指导。
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| 关 键 词： | 飞行特性 过渡飞行 悬停 小速度前飞 |
| 文章编号： | 1000-6893(1999)05-0455-03 |
FLIGHT CHARACTERISTICS OF HELICOPTER FROM HOVER TO FORWARD FLIGHT |
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| XIONG Liang-yu,XIANG Jin-wu.FLIGHT CHARACTERISTICS OF HELICOPTER FROM HOVER TO FORWARD FLIGHT[J].Acta Aeronautica et Astronautica Sinica,1999,20(5):455-457. |
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| Authors: | XIONG Liang-yu XIANG Jin-wu |
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| Institution: | Institute of Aircraft Design, Beijing University of Aeronautics &; Astronautics, Beijing 100083, China |
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| Abstract: | A model is described in this paper, which is used to discuss the changes of the flight height and velocity during the transient flight from hover to forward flight of a helicopter. First, the calculation method is given, the results of which are validated against the flight data of an example SA365N. Finally, for general helicopters, some useful results are provided in various control inputs and states of engine breakdown. The conclusions can be used as references to the pilot in flight. |
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| Keywords: | flight characteristics transient flight hover low speed forward flight |
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