Effects of distributed leading-edge roughness on aerodynamic performance of a low-Reynolds-number airfoil: an experimental study
ABSTRACT: Distributed leading-edge (LE) roughness could have significant impact on the aerodynamic performance of a low-Reynolds-number (low-Re) airfoil, which has not yet been fully understood. In the present study, experiments were conducted to study the effects of distributed hemispherical roughn...
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| Format: | Article |
| Language: | English |
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Elsevier
2018-05-01
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| Series: | Theoretical and Applied Mechanics Letters |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2095034918301107 |