航天器环境工程2018，Vol.35Issue(1)：7-13,7.DOI:10.3969/j.issn.1673-1379.2018.01.002
梯度波纹夹层防护结构超高速碰撞特性仿真研究
Simulation of hypervelocity impact characteristics of gradient corrugated-core sandwich plates
摘要
Abstract
In view of the demand of the protection of the spacecraft against the orbital debris, a gradient corrugated-core sandwich bumper shield under hypervelocity impact is numerically studied. It can be seen that the propagation of the shock wave in the gradient corrugated-core sandwich bumper shield is more complicated than that in the Whipple shield, and that is more conducive for the crush of the orbital debris. With the increase of the impact velocity from 5 to 20 km/s, the expansion angle of the debris cloud increases firstly and then decreases. Furthermore, it is shown that the front corrugated-core absorbs most impact energy of the debris. The research can help the design of the orbital debris shield.关键词
空间碎片/梯度波纹夹层结构/超高速碰撞/碎片云特性/舱壁损伤特性/仿真研究Key words
orbital debris/gradient corrugated-core sandwiches/hypervelocity impact/debris cloud characteristics/rear wall damage characteristics/simulation study分类
数理科学引用本文复制引用
邓泽华,郭锐,周昊,唐生勇..梯度波纹夹层防护结构超高速碰撞特性仿真研究[J].航天器环境工程,2018,35(1):7-13,7.基金项目
中央高校基本科研业务费专项资金项目(编号:30915118821) （编号:30915118821）
上海航天SAST基金项目(编号:SAST201521) （编号:SAST201521）
2015年度CAST-BISEE创新基金项目 （）
