Evaluation of aerodynamic coefficients of supercritical airfoil NASA sc(2) 0712: A comparative study of 2D and 3D flow models with experimental validations

Evaluation of aerodynamic coefficients of supercritical airfoil NASA sc(2) 0712: A comparative study of 2D and 3D flow models with experimental validations

This study presents a comparative numerical analysis of 2D and 3D compressible, turbulent flows around the supercritical airfoil NASA sc(2) 0712 at Mach number M = 0.5 using the finite volume method implemented in ANSYS Fluent, focusing on the estimation of drag coefficients in relation to existing...

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Bibliographic Details
Main Authors: Šukunda Teodora, Svorcan Jelena, Ivanov Toni
Format: Article
Language:English
Published: University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2025-01-01
Series:FME Transactions
Subjects:
supercritical airfoil
drag coefficient
cfd
poly mesh
mosaic elements
3d versus 2d
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2025/1451-20922501105Q.pdf
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