Numerical and experimental study of the impact on aerodynamic characteristics of the NACA0012 airfoil
Using computational models and low-speed wind tunnel tests, the aerodynamic characteristics of the NACA 0012 airfoil with low Re numbers of (8 × 104{10}^{4}, 2 × 105{10}^{5}, 3 × 105{10}^{5}, and 4 × 105){10}^{5}) and angle of attack (AOA) ranging from 0° to 18° by two steps are examined. Using the...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
De Gruyter
2024-02-01
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| Series: | Open Engineering |
| Subjects: | |
| Online Access: | https://doi.org/10.1515/eng-2022-0506 |