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...

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发表在:International Journal of Emerging Technology and Advanced Engineering
主要作者: Hamid A.H.A.; Mohamad F.; Noh M.H.M.; Nasir R.E.M.; Sapardi M.A.M.
格式: 文件
语言:English
出版: IJETAE Publication House 2022
在线阅读:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85145034334&doi=10.46338%2fijetae1222_02&partnerID=40&md5=6b108eaf47cf6e862a4bb20084bdcb88