Parametric Optimization of NACA 4412 Airfoil in Ground Effect Using Full Factorial Design of Experiment
This investigation emphasizes the changes of the lift-to-drag ratio of an airfoil with the variation of ground clearance and angles of attack. Various ground clearances and angles of attack with a fixed speed of 30 m/s are applied to the NACA 4412 airfoil. Computational fluid dynamics (CFD) is used...
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| Main Authors: | , |
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| Format: | Article |
| Published: |
2022
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| Subjects: | |
| Online Access: | https://repository.li.mahidol.ac.th/handle/123456789/76967 |
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| Institution: | Mahidol University |