A CFD Assessment to Subsonic Flow Around NACA4412
The purpose of this study is determined values of Mach Number (Ma) for Subsonic flow around NACA4412 which is begun shock wave and known the location it. A 2-dimensional triangular C-type grid is used to match the reference measurements at an airfoil cross-section was taken from NACA 4412 from lead...
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| Format: | Article |
| Language: | Arabic |
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Mustansiriyah University/College of Engineering
2011-12-01
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| Series: | Journal of Engineering and Sustainable Development |
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| Online Access: | https://jeasd.uomustansiriyah.edu.iq/index.php/jeasd/article/view/1315 |