Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method

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Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method

The comparison between incompressible and compressible flow for aerodynamic coefficients and flow characteristics has been made for NACA 2412 airfoil. The FEM is used to obtain results. The fluid domain of 10C has been constructed to initialize the boundary conditions of incompressible and compressi...

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Bibliographic Details
Main Authors:	Kharulaman, Liyana, Aabid, Abdul, Mehaboobali, Fharukh Ahmed Ghasi, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Blue Eyes Intelligence Engineering & Sciences Publication 2019
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/75891/ http://irep.iium.edu.my/75891/1/Liyana-paper.pdf http://irep.iium.edu.my/75891/7/75891_Research%20onFlows%20for%20NACA%202412%20%20airfoil%20_scopus.pdf

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