Aerodynamic Profile Modification of a NACA 0012 Aerofoil for Enhanced Lift-Drag Characteristics at Low Reynolds Number

Aerodynamic Profile Modification of a NACA 0012 Aerofoil for Enhanced Lift-Drag Characteristics at Low Reynolds Number

This article discusses the enhanced lift-drag ratio of a geometrically modified National Advisory Committee for Aeronautics 0012 aerofoil at a low Reynolds number of 40000. The study involves validating the Reynolds Averaged Navier Stokes Transition Shear Stress Transport model for the analysis of f...

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Bibliographic Details
Main Authors: Anupam Krishnan, Sukanta Roy
Format: Article
Language:English
Published: Universidade do Porto 2022-04-01
Series:U.Porto Journal of Engineering
Subjects:
naca 0012
small-scale wind turbine blade
transition sst
rans simulation
low reynolds number aerofoil
Online Access:https://journalengineering.fe.up.pt/index.php/upjeng/article/view/1174

Internet

https://journalengineering.fe.up.pt/index.php/upjeng/article/view/1174

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