仿翼龙滑翔机的气动性能分析
Aircraft Design(2016)
Abstract
针对某翼龙仿形电动滑翔机飞机的研制,采用涡格法气动软件AVL建立了飞机的气动分析模型,理论计算了该飞机的升力、阻力与俯仰力矩系数,讨论了相应的气动特性,以论证该翼龙滑翔机设计的合理性.试飞与分析结果表明,本文的仿翼龙滑翔机的设计方案是成功的,该飞机具有出色的气动特性.
MoreAI Read Science
Must-Reading Tree
Example
![](https://originalfileserver.aminer.cn/sys/aminer/pubs/mrt_preview.jpeg)
Generate MRT to find the research sequence of this paper
Chat Paper
Summary is being generated by the instructions you defined