Comparative tests of thick and thin turning vanes in the royal aircraft establishment 4 X 3-ft wind tunnel

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dc.contributor.author K. G. Winter en_US
dc.date.accessioned 2014-10-21T15:51:00Z
dc.date.available 2014-10-21T15:51:00Z
dc.date.issued 1947 en_US
dc.identifier.other ARC/R&M-2589 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3044
dc.description.abstract The tests were made by replacing the existing centre six thick vanes at the first corner of the 4 x 3-ft wind tunnel by vanes of sheet metal. The thin vanes reduced the-corner loss, estimated from a wake traverse behind one vane, without any deterioration in outflow, and are therefore recommended for use in future wind tunnels. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Comparative tests of thick and thin turning vanes in the royal aircraft establishment 4 X 3-ft wind tunnel en_US


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