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...
類似資料
-
Aerodynamic performance of dragonfly-inspired wings in gliding flight for varying angle of attack and Reynolds number: a numerical study
著者:: Verekar P.; Baloor S.S.; Yusoff H.; Magami I.A.B.; Kamangar S.; Zuber M.
出版事項: (2025) -
Aerodynamic performance of dragonfly-inspired wings in gliding flight for varying angle of attack and Reynolds number: a numerical study
著者:: Verekar, 等
出版事項: (2025) -
Computational Aerodynamic Investigations on Wash Out Twist Morphing MAV Wings
著者:: Ismail N.I.; Tasin M.A.; Sharudin H.; Basri M.H.; Mat S.C.; Yusoff H.; Nasir R.E.M.
出版事項: (2022) -
Flow past two interlocking squares cylinder at low reynolds number
著者:: 2-s2.0-85047662480
出版事項: (2018) -
Optimization of a Blended-Wing-Body Unmanned Aerial Vehicle Design for Maximum Aerodynamic Lift-to-Drag Ratio
著者:: 2-s2.0-85148520567
出版事項: (2023)