| 某型机后机身平尾颤振模型设计刚度模拟的探讨 |
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| 引用本文： | 罗家泉.某型机后机身平尾颤振模型设计刚度模拟的探讨[J].南京航空航天大学学报,1991(2). |
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| 作者姓名： | 罗家泉 |
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| 作者单位： | 南京航空学院空气动力学系 |
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| 摘 要： | 本文探讨了飞机低速颤振模型刚度模拟计算的一种方法。用此方法对某种型号飞机的后机身、平尾刚度进行设计计算,试验结果表明,这种计算方法是可行的。
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| 关 键 词： | 机身 水平尾翼 颤振试验 刚度模拟 |
A Study on the Stiffness Simulation Calculation Method of Flutter Models of After Body and Horizontal Tail of a New Type Aeroplane |
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| Luo Jiaguan.A Study on the Stiffness Simulation Calculation Method of Flutter Models of After Body and Horizontal Tail of a New Type Aeroplane[J].Journal of Nanjing University of Aeronautics & Astronautics,1991(2). |
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| Authors: | Luo Jiaguan |
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| Institution: | Department of Aerodynamics |
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| Abstract: | In this paper a stiffness simulation calculation method of low speed flutter models of an aeroplane is studied. Using this method, the after body and the horizontal tail of a new type aeroplane are calculated. Experimental results show that the method is feasible. |
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| Keywords: | fuselages horizontal tails flutter test stiffness simulation |
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