计算航空器起落架起转、回弹载荷的解析方法 |
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引用本文: | 杨俊严.计算航空器起落架起转、回弹载荷的解析方法[J].直升机技术,1998(3). |
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作者姓名: | 杨俊严 |
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作者单位: | 中国直升机设计研究所 景德镇 |
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摘 要: | 本文是对文献1]的补充。文献1]中给出的公式,仅适用于t_p≤t_(max)情况。对于t_p>t(max),需另行推导计算公式。本文在文献1]的假设及公式基础上,导出了适用于t_p>t_(max)的公式,并对其应用及有关问题进行了讨论。最后给出了算例结果。
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关 键 词: | 起落架 起转、回弹载荷 解析方法 |
ANALYTICAL METHOD OF CALCULATION SPIN-UP AND SPRING-BACK LOADS OF AIRCRAFT LANDING GEAR |
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Authors: | Yang Junyan |
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Abstract: | This is additional material of reference1] .Formula given in reference1] only applies to condition for tptmax another formula should be deducted.On the basis of hypothesis and formula in reference1] ,a formula has been deducted which applies to condition tp>tmax and its application and regard problem have beem discussed.In the end of this paper,exemplary result is given. |
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Keywords: | landing gear spin-up and spring-back loads analytical method |
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