一种在高超声速条件下展开的充气翼  

A Kind of Inflatable Wing Which can Unfold Under Hypersonic Condition

作　　者：陈旭[1,2] 冯昊 武士轻[1,2] Chen Xu;Feng Hao;Wu Shiqing(Beijing Institute of Space Mechanics&Electricity,Beijing 100094,China;Laboratory of Aerospace Entry,Descent and Landing Technology,China Aerospace Science and Technology Corporation,Beijing 100094,China)

机构地区：[1]北京空间机电研究所,北京100094 [2]中国航天科技集团有限公司航天进入减速与着陆技术实验室,北京100094

出　　处：《气动研究与试验》2024年第5期89-97,共9页Aerodynamic Research & Experiment

摘　　要：针对一种在高超声速飞行条件下展开的充气翼进行了研究。分析了充气翼结构布局对变形情况和应力分布的影响,设计了能够从狭小的翼舱内展开的折叠方案。对充气翼在高超声速来流条件下的热流情况进行了分析,通过仿真计算给出了柔性防热材料方案。最后,通过充气翼结构原理样机的地面充气展开试验,验证了结构布局和折叠方案的可行性。A kind of inflatable wing which can unfold under hypersonic condition is researched.The influence on deformation and stress distribution by inflatable wing structure layout is analyzed.Folding method of unfolding from narrow wing cabin is designed.The heat flow under hypersonic condition is analyzed.And flexible heat protection material is designed by simulation.Finally,the inflatable wing structure prototype is tested on ground condition,which can verify the feasibility of structure layout and folding method.

关 键 词：充气翼 高超声速 折叠/展开 柔性防热材料 

分 类 号：V45[一般工业技术—材料科学与工程]