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。
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].
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1989年第1期46-50,共5页
Journal of Astronautics
关键词
航天器
气动力计算
弹性发散
Space vehicle, Aerodynamics, Aerodynamic Computation, Aerodynamic interence.
