飞行器折叠翼展开冲击环境条件研究
Research on Environmental Conditions of Aircraft Folding Wing Spread Shock
李亚南 1韦冰峰 1肖健 1张永杰 1崔洪伟1
作者信息
- 1. 北京强度环境研究所,北京 100076
- 折叠
摘要
带折叠翼飞行器在结构上与传统飞行器略有差异,其翼展开冲击环境条件的制定无相似型号及经验可参考.本文针对飞行器折叠翼展开冲击环境条件问题,通过分析五种条件制定方法,对不同样本量情况下飞行器折叠翼展开冲击环境进行研究,给出了该类型飞行器折叠翼展开冲击环境条件的制定方法.
Abstract
The structure of the aircraft with folding wing is different from that of the traditional aircraft.There is no similar model or experience for reference in the making of shock environmental conditions for the deployment of aircraft wing.Aiming at the formulation of environmental conditions of aircraft wing spread shock,this paper analyzes five conditions formulation methods to research on environmental conditions of aircraft wing spread shock under different sample sizes.The method of setting up the shock environment condition of aircraft wing is given.
关键词
飞行器折叠翼展开/冲击环境/条件制定Key words
aircraft folding wing spread/shock environmental/formulation of conditions引用本文复制引用
出版年
2024
NETL
NSTL
万方数据