| 从非稳态飞行中确定飞机的纵向平衡曲线 |
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| 引用本文： | 樊力,张勇.从非稳态飞行中确定飞机的纵向平衡曲线[J].飞行力学,1993,11(2):89-97. |
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| 作者姓名： | 樊力 张勇 |
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| 作者单位： | 飞行试验研究院，飞行试验研究院 西安 710089，西安 710089 |
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| 摘 要： | 介绍了俄罗斯飞行研究院广泛应用的从非稳态飞行中确定飞机纵向平衡曲线的试飞方法。该方法具有对试飞员动作要求宽、每个动作所包含的信息量大、节省起落、缩短试飞周期的优点。同时,还就该方法所存在的不足进行了讨论。
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| 关 键 词： | 飞行试验 非稳态飞行 平衡曲线 |
THE METHOD DETERMINING THE LONGTUDINAL TRIMCURVE OF THE AIRPLANE FROM NON-STEADY FLIGHT |
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| Fan Li,Zhang Yong.THE METHOD DETERMINING THE LONGTUDINAL TRIMCURVE OF THE AIRPLANE FROM NON-STEADY FLIGHT[J].Flight Dynamics,1993,11(2):89-97. |
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| Authors: | Fan Li Zhang Yong |
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| Institution: | Chinese Flight Test Establishment |
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| Abstract: | This paper introduces a new flight test method determing the Longtudinal trim curve of the airplane from non-steady flight. The method has been widely used by the Russia Flight Research Institute. It has the advantages of simple inputs with large quantity information, saving sorties, shortening the flight test period. The deficiencies of the method are also discussed. |
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| Keywords: | Flight test Non-steady flight Trim curve |
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