摘要
本文介绍了一种玻璃钢蒙皮 /全腔填充泡沫塑料夹芯的小型无人机机翼的设计方法。
This article introduces the design method of an UAV's wing with FRP foam sandwich structure. The wing needs to satisfy the special operation requirements for water proof and sea floating.
出处
《玻璃钢/复合材料》
CAS
CSCD
2003年第1期17-20,共4页
Fiber Reinforced Plastics/Composites