Flow structure and vorticity transport on a plunging wing
The structure and dynamics of the flow field created by a plunging flat plate airfoil are investigated at a chord Reynolds number of 10,000 while varying plunge amplitude and Strouhal number. Digital particle image velocimetry measurements are used to characterize the shedding patterns and the inter...
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| Format: | Others |
| Language: | English |
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University of Iowa
2014
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| Online Access: | https://ir.uiowa.edu/etd/4623 https://ir.uiowa.edu/cgi/viewcontent.cgi?article=5139&context=etd |