| 细长飞行器的气动弹性发散分析 |
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| 引用本文： | 陈文俊.细长飞行器的气动弹性发散分析[J].宇航学报,1989(1):46-50. |
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| 作者姓名： | 陈文俊 |
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| 作者单位： | 北京精密机械总体设计部 |
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| 摘 要： | 本文从下列两方面推广文献1]中的二升力火箭弹体气动弹性发散分析:一是把两个集中升力扩大到任意个集中升力;二是计及空气动力干扰效应。
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| 关 键 词： | 航天器 气动力计算 弹性发散 |
ANALYSIS OF AEROELASTIC DIVERGENCE FOR THE SLENDER FLIGHT VEHICLES |
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| Chen Wenjun.ANALYSIS OF AEROELASTIC DIVERGENCE FOR THE SLENDER FLIGHT VEHICLES[J].Journal of Astronautics,1989(1):46-50. |
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| Authors: | Chen Wenjun |
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| Institution: | Beijing Precision Machinery Overall Design |
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| Abstract: | This paper generalizes the aeroelastic divergence analysis of a rocket applied by two point aerodynamic lifts in reference 1] in two senses, to extend the number of the point aerodynamic lifts on a slender flight vehile from 2 to N (arbitrary positive integral) and include the effect of aerodynamic interfere omitted in 1]. |
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| Keywords: | Space vehicle Aerodynamics Aerodynamic Computation Aerodynamic interence |
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