海军航空工程学院学报2017，Vol.32Issue(5)：443-446,4.DOI:10.7682/j.issn.1673-1522.2017.05.005
低雷诺数下小型无人机翼型气动特性分析
Aerodynamic Characteristics Analysis of the Small Unmanned Aerial Vehicle's Airfoil at Low Reynolds Numbers
摘要
Abstract
Based on the research of small UAV,numerical simulations of the flow over airfoil CLARKY Re=1.0×105、5× 105、1.0×106were used to analyze the aerodynamic performances -5°~20° in a range of low Reynolds numbers with the transition model eNof linear stability theory.The results showed that the airflow separation was gradually transformed into a laminar separation bubble structure from completely separation,while the transition position on the upper surface of the airfoil was moved toward leading edge continuously with the increase of Reynolds number,and the aerodynamic character?istics of airfoil CLARKY was gradually improved.关键词
小型无人机/低雷诺数/翼型/气动特性Key words
small UAV/low Reynolds number/airfoil/aerodynamic characteristics分类
航空航天引用本文复制引用
康小伟,李冰,郭卫刚..低雷诺数下小型无人机翼型气动特性分析[J].海军航空工程学院学报,2017,32(5):443-446,4.
