| 副翼配重的着陆冲击响应 |
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| 引用本文： | 黄树春,汪长元.副翼配重的着陆冲击响应[J].航空学报,1992,13(8):427-430. |
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| 作者姓名： | 黄树春 汪长元 |
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| 作者单位： | 哈尔滨飞机制造公司设计所，哈尔滨飞机制造公司设计所 哈尔滨 150066，哈尔滨 150066 |
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| 摘 要： | 提供了一个计算副翼配重着陆冲击响应的方法。由于主起落架为纯摇臂式,考虑机体的弹性,机体和主起落架运动联立求解的加速度不是显式,因此必须用高斯方法解加速度的线性方程组,再用吉尔方法解微分方程。
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| 关 键 词： | 动力响应 着陆冲击 摇臂 |
DYNAMIC RESPONSE OF THE AILERON BALANCE WEIGHT DURING LANDING IMPACT |
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| Huang Shu-chun,Wang Chang-yuan.DYNAMIC RESPONSE OF THE AILERON BALANCE WEIGHT DURING LANDING IMPACT[J].Acta Aeronautica et Astronautica Sinica,1992,13(8):427-430. |
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| Authors: | Huang Shu-chun Wang Chang-yuan |
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| Institution: | Harbin Aircraft Manufacturing Corporation, Harbin, 150066 |
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| Abstract: | A method of calculating dynamic response of the aileron balance weight during landing impact is presented in this paper. Because the main landing gear of the investigated airplane is a type of pure rocker arm, as well as airframe elasticity is considered, airplane motion and main landing gear motion are simultaneously solved, and the accelerations are implicit in the motion equations, Gill method can not be used directly. fortunately, the motion equations are linear equations about the accelerations. The linear equations for the accelerations can be solved by Gauss main element deletion method and the accelerations will be obtained. The differential equation will be solved by Gill method. |
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| Keywords: | dynamic response landing impact rocker arm type |
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