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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:	Krishnan, Anupam, Roy, Sukanta
Format:	Journal Article
Published:	University of Porto 2022
Online Access:	http://hdl.handle.net/20.500.11937/88567

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