摘要
为满足UAV机翼的结构强度及隐身要求,机翼采用全复合材料结构,在目前的无人机机翼结构的材料性能、载荷等条件下,对机翼进行了静强度及动力学分析,通过应用有限元分析软件和计算软件对全复合材料机翼进行了建模和静强度分析与动力学分析。
In order to satisfy wing structural strength and stealth requirement, all composites wings were chose to analyze static intensity and dynamics. The wing was made static intensity and dynamics analysis for structural strength and load condition of actual new wing. Also we have made modeling ,static strength and dynamics analysis with finite element analysis＇ s software and Computation＇s software.
出处
《强度与环境》
2009年第6期40-44,共5页
Structure & Environment Engineering
