| 固定小翼颤振激励系统试飞验证 |
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| 引用本文： | 霍幸莉,周友明,李勤红.固定小翼颤振激励系统试飞验证[J].飞行力学,2009,27(4). |
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| 作者姓名： | 霍幸莉 周友明 李勤红 |
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| 作者单位： | 中国飞行试验研究院,飞机所,陕西,西安,710089 |
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| 摘 要： | 针对一种新研制的带开缝旋转圆筒固定小翼激励系统,对其工作特性和激励力特性进行了试飞验证。试验结果表明,该系统工作特性基本达到了最初的设计指标要求,激励力特性理论计算与实测结果基本吻合,为该系统进一步的应用奠定了基础。
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| 关 键 词： | 带开缝旋转圆筒固定小翼 颤振激励系统 激励力特性 飞行试验 |
Flight Test of a Fixed Vane Flutter Excitation System |
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| HUO Xing-li,ZHOU You-ming,LI Qin-hong.Flight Test of a Fixed Vane Flutter Excitation System[J].Flight Dynamics,2009,27(4). |
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| Authors: | HUO Xing-li ZHOU You-ming LI Qin-hong |
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| Institution: | Aircraft Flight Test Technology Institute;CFTE;Xi'an 710089;China |
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| Abstract: | Operational abilities and excitation force characteristics of a new national trailing-edge fixed-vane excitation system(FVES) with a slotted rotating cylinder were verified by flight tests.The test results show that its operational abilities are satisfied with the primary designed requirements and the theory analysis forces characteristics are almost the same as measured results,which provide the further application foundation of the FVES. |
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| Keywords: | trailing-edge fixed-vane with a slotted rotating cylinder flutter excitation system excitation force characteristics flight test |
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