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Experimental study of the wake-modes...
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Buzard, Alan Joe.
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Experimental study of the wake-modes for propulsion of two-dimensional heaving airfoils.
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Experimental study of the wake-modes for propulsion of two-dimensional heaving airfoils./
作者:
Buzard, Alan Joe.
面頁冊數:
49 p.
附註:
Source: Masters Abstracts International, Volume: 43-05, page: 1791.
Contained By:
Masters Abstracts International43-05.
標題:
Engineering, Marine and Ocean. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1425444
ISBN:
049697159X
Experimental study of the wake-modes for propulsion of two-dimensional heaving airfoils.
Buzard, Alan Joe.
Experimental study of the wake-modes for propulsion of two-dimensional heaving airfoils.
- 49 p.
Source: Masters Abstracts International, Volume: 43-05, page: 1791.
Thesis (M.S.)--Florida Atlantic University, 2005.
Particle image velocimetry and flow visualization are used to characterize the wake of a heaving airfoil in a set of two experiments. In the first experiment a tandem airfoil configuration is used, with a stationary airfoil downstream of a heaving airfoil (modified Schmidt wave-propeller). Several vortex structures are identified for a forced Strouhal number (St)---based on airfoil chord-length, forcing frequency, and free-steam velocity---for 0.1 < St < 0.7. An asymmetric average velocity profile is measured in the upper St range. In the second experiment, the wake behind a single heaving airfoil is further inspected, with the purpose of highlighting the asymmetric wake, for 0.1 < St < 1.0. A maximum wake excursion of 18 degrees is measured at St = 0.6, and a minimum excursion of 5.7 degrees occurs at St = 0.9. Using averaged velocity profiles, a virtual origin of the wake excursion is also calculated.
ISBN: 049697159XSubjects--Topical Terms:
1019064
Engineering, Marine and Ocean.
Experimental study of the wake-modes for propulsion of two-dimensional heaving airfoils.
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Source: Masters Abstracts International, Volume: 43-05, page: 1791.
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Particle image velocimetry and flow visualization are used to characterize the wake of a heaving airfoil in a set of two experiments. In the first experiment a tandem airfoil configuration is used, with a stationary airfoil downstream of a heaving airfoil (modified Schmidt wave-propeller). Several vortex structures are identified for a forced Strouhal number (St)---based on airfoil chord-length, forcing frequency, and free-steam velocity---for 0.1 < St < 0.7. An asymmetric average velocity profile is measured in the upper St range. In the second experiment, the wake behind a single heaving airfoil is further inspected, with the purpose of highlighting the asymmetric wake, for 0.1 < St < 1.0. A maximum wake excursion of 18 degrees is measured at St = 0.6, and a minimum excursion of 5.7 degrees occurs at St = 0.9. Using averaged velocity profiles, a virtual origin of the wake excursion is also calculated.
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http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1425444
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