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飞行器折叠翼展开冲击环境条件研究

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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.
Research on Environmental Conditions of Aircraft Folding Wing Spread Shock
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.

aircraft folding wing spreadshock environmentalformulation of conditions

李亚南、韦冰峰、肖健、张永杰、崔洪伟

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北京强度环境研究所,北京 100076

飞行器折叠翼展开 冲击环境 条件制定

2024

强度与环境
北京强度环境研究所

强度与环境

CSTPCD
影响因子:0.45
ISSN:1006-3919
年,卷(期):2024.51(2)
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