| 可动平尾对直升机纵向飞行品质的影响 |
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| 引用本文： | 方景龙,胡启元.可动平尾对直升机纵向飞行品质的影响[J].飞行力学,1997,15(1):71-75. |
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| 作者姓名： | 方景龙 胡启元 |
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| 作者单位： | 中国直升机设计研究所!景德镇，333001 |
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| 摘 要： | 简单介绍了直升机纵向飞行品质对平尾设计的基本要求，提出了可动平尾的设计思想，概述了直升机的可动平尾的工作原理及其工作环境。然后主要分析了可动平尾对直升机纵向飞行品质的有利影响，其中包括可动平尾的“主动控制”能力、“低速配平”能力和“总距配平”能力。分析表明，可动平尾设计是直升机构型造反和初始设计时一个较理想的方案。
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| 关 键 词： | 直升机 飞行品质 可动平尾 |
The Influence of Movable Stabilator on Helicopter Longitudinal Flying Qualities |
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| Fang Jinglong,Hu Qiyuan.The Influence of Movable Stabilator on Helicopter Longitudinal Flying Qualities[J].Flight Dynamics,1997,15(1):71-75. |
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| Authors: | Fang Jinglong Hu Qiyuan |
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| Institution: | Chinese Helicopter Research and Development Institute |
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| Abstract: | This paper introduced helicopter's movable stabilator and its poor environment. It then analyzed good Influence of movable stabilator on helicopter longitudinal f lying qualities. Finally, a conclusion is given: movable stabilator is a good configuration during the period of helicopter preliminary aerodynamic design. |
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| Keywords: | Helicopter Flying qualities Movable stabilator |
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