Aerodynamics of an airfoil with leading‐edge icing
Abstract The flow over the leading edge of an NREL S826 reference airfoil with three different icing‐inspired leading‐edge contamination geometries has been assessed experimentally. Particle image velocimetry was performed on the leading edge of the airfoil for a range of angles‐of‐attack between −4...
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| Glavni autori: | , |
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| Format: | Artigo |
| Jezik: | Inglês |
| Izdano: |
Wiley
2021-08-01
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| Serija: | Wind Energy |
| Teme: | |
| Online pristup: | https://doi.org/10.1002/we.2603 |
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