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运载火箭1/5动力学缩比模型设计

刘财芝 唐国金 周利霖

国防科技大学学报2017,Vol.39Issue(2):27-31,5.
国防科技大学学报2017,Vol.39Issue(2):27-31,5.DOI:10.11887/j.cn.201702004

运载火箭1/5动力学缩比模型设计

1/5 dynamic scaled model design of launch vehicle

刘财芝 1唐国金 2周利霖1

作者信息

  • 1. 国防科技大学 航天科学与工程学院, 湖南 长沙 410073
  • 2. 北京宇航系统工程研究所, 北京 100076
  • 折叠

摘要

Abstract

The design of dynamic scale model is one of the most important parts in the scale model test which is an effective approach to obtain dynamic characteristics of large launch vehicle.Taking the launch vehicle as the object, the similarity relationships for each part were derived on the basis of the structural components of the launch vehicle.Transverse dynamic similarity relationships of the launch vehicle were derived by taking advantage of the consistent similarity in respect of transverse stiffness and mass.Taking the actual processing and manufacturing conditions into consideration, the restrictions of similarity coefficient for transverse stiffness and mass were analyzed.According to the relationships and the restrictions above, a 1/5 dynamic scale model was designed and its similarity of dynamic characteristics was verified through the numerical analysis of finite element.The verification result shows that the 1/5 scale model gets a high-level similarity with the prototype in terms of dynamic characteristics, and the method can be effectively applied to the design of dynamic scale model for launch vehicle.

关键词

运载火箭/相似理论/缩比模型/动力学特性

Key words

launch vehicle/similitude theory/scale model/dynamic characteristics

分类

航空航天

引用本文复制引用

刘财芝,唐国金,周利霖..运载火箭1/5动力学缩比模型设计[J].国防科技大学学报,2017,39(2):27-31,5.

基金项目

国家自然科学基金资助项目(11472003) (11472003)

国防科技大学学报

OA北大核心CSCDCSTPCD

1001-2486

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