Effects of porous tunnel walls on high lift airfoil testing
When a model is tested in a wind tunnel of either open or closed boundaries, the flow field around the model is modified, so that the results of a wind tunnel test do not exactly correspond to flight results. In order to obtain reliable wind tunnel data, wall corrections must be known accurately or...
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| Language: | English |
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University of British Columbia
2011
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| Online Access: | http://hdl.handle.net/2429/34871 |