The 9 x 3 in. induced-flow high-speed wind tunnel at the national physical laboratory

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dc.contributor.author D. W. Holder en_US
dc.contributor.author R. J. North en_US
dc.date.accessioned 2014-10-21T15:52:49Z
dc.date.available 2014-10-21T15:52:49Z
dc.date.issued 1949 en_US
dc.identifier.other ARC/R&M-2781 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3332
dc.description.abstract A 9 X 3 in. high-speed wind tunnel driven by a compressed-air injector has been built in the Aerodynamics Division of the National Physical Laboratory. The tunnel operates at roughly atmospheric stagnation pressure and has so far been used to give Mach numbers up to 1.8. The general arrangement of the tunnel and the preliminary calibration, which is generally satisfactory, are described. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The 9 x 3 in. induced-flow high-speed wind tunnel at the national physical laboratory en_US


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