Formation and Detachment of Leading Edge Vortices on Unsteady Airfoils
The unsteady velocity field around a pitching and plunging airfoil has been investigated whereby two different mechanisms leading to the detachment of leading edge vortices, which form at the suction side of the airfoil during a motion cycle, were of central interest. One of these mechanisms is anal...
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| Format: | Others |
| Language: | German en |
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2015
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| Online Access: | https://tuprints.ulb.tu-darmstadt.de/4670/7/Thesis_korrigiert_final_3.pdf Widmann, Alexander Guido Martin <http://tuprints.ulb.tu-darmstadt.de/view/person/Widmann=3AAlexander_Guido_Martin=3A=3A.html> (2015): Formation and Detachment of Leading Edge Vortices on Unsteady Airfoils.Darmstadt, Technische Universität, [Ph.D. Thesis] |
Internet
https://tuprints.ulb.tu-darmstadt.de/4670/7/Thesis_korrigiert_final_3.pdfWidmann, Alexander Guido Martin <http://tuprints.ulb.tu-darmstadt.de/view/person/Widmann=3AAlexander_Guido_Martin=3A=3A.html> (2015): Formation and Detachment of Leading Edge Vortices on Unsteady Airfoils.Darmstadt, Technische Universität, [Ph.D. Thesis]