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...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/75891/ http://irep.iium.edu.my/75891/ 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 |