Hochschulschrift
Development, control and recovery of leading- and trailing-edge vortices in tandem-airfoil configurations
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Extent
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Online-Ressource
- Language
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Englisch
- Notes
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Darmstadt, Techn. Univ., Diss., 2009
- Creator
- URN
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urn:nbn:de:tuda-tuprints-19290
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 10:52 AM CEST
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Object type
- Hochschulschrift
Associated
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Control of leading edge separation on an airfoil by localized excitation
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Study on relationship between the geometry of Leading and Trailing Edges of Airfoil and their Aeroacoustics Parameters at low Reynolds number
Aerodynamic behavior of an airfoil with morphing trailing edge for wind turbine applications
Investigation of blunt trailing edge noise from an asymmetric airfoil under different aerodynamic loads
Investigation of blunt trailing edge noise from an asymmetric airfoil under different aerodynamic loads
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