Flow Past an Airfoil with a Leading-Edge Rotation Cylinder
A study was undertaken to measure and characterize the effects of a leading-edge rotating cylinder on the growth, development, and separation of the boundary layer and the wake structure.
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Veröffentlicht in: | Journal of aircraft 2002-11, Vol.39 (6), p.1079-1084 |
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Hauptverfasser: | , , , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | A study was undertaken to measure and characterize the effects of a leading-edge rotating cylinder on the growth, development, and separation of the boundary layer and the wake structure. |
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ISSN: | 0021-8669 1533-3868 |
DOI: | 10.2514/2.3040 |