Design of low Reynolds number airfoil for micro aerial vehicle
V. Somashekar,A. Immanuel Selwyn Raj +1 more
- Vol. 376, Iss: 1, pp 012046
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The article was published on 2018-06-01 and is currently open access. It has received 4 citations till now. The article focuses on the topics: Reynolds number & Airfoil.read more
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Numerical and experimental study of the laminar separation bubble over SS007 airfoil for micro aerial vehicles
TL;DR: In this article, the laminar separation bubble (LSB) characteristics of SS007 airfoil at the chord Reynolds number of Rec = 0.68 to 0.28 were investigated and a cell-centred control volume space discretisation approach was used to solve the governing equations of the flow.
Journal ArticleDOI
Numerical Investigation for Selection of Airfoil with Regard to Flying Wing Applications
Journal ArticleDOI
Aerodynamic Simulation and Optimization of Micro Aerial Vehicle Rotor Airfoil at Low Reynolds Number
TL;DR: In this article , the aerodynamic simulation and optimization of NACA 0012 airfoil at a low Reynolds number using unsteady Reynolds-averaged Navier-Stokes (URANS) and Spalart-Allmaras turbulence model in Ansys Fluent was described.
Journal ArticleDOI
Aerodynamic and bending analysis of low-speed airfoils at high reynold number
TL;DR: In this paper , a computational analysis was carried to find out the most suitable airfoil design at a low Reynolds number based on aerodynamic and mechanical properties for low-speed fixed-wing UAVs.
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Journal ArticleDOI
Numerical and experimental study of the laminar separation bubble over SS007 airfoil for micro aerial vehicles
TL;DR: In this article, the laminar separation bubble (LSB) characteristics of SS007 airfoil at the chord Reynolds number of Rec = 0.68 to 0.28 were investigated and a cell-centred control volume space discretisation approach was used to solve the governing equations of the flow.