Aerodynamics of a Modified High-Lift Low Reynolds Number Airfoil: Preliminary Analysis
Airfoil selection is a crucial phase in the design of a small unmanned fixed-wing aircraft to allow a minimum size and weight of the lifting surfaces. The present study analyzesairfoils to be used in low operating Reynolds number unmanned aerial vehicles (UAV) using XFLR5 software, which was validat...
| 出版年: | International Journal of Emerging Technology and Advanced Engineering |
|---|---|
| 第一著者: | |
| フォーマット: | 論文 |
| 言語: | English |
| 出版事項: |
IJETAE Publication House
2022
|
| オンライン･アクセス: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85145034334&doi=10.46338%2fijetae1222_02&partnerID=40&md5=6b108eaf47cf6e862a4bb20084bdcb88 |