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The Vertical Wind Tunnel of the National Advisory Committee for AeronauticsThe vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described in this report. The tunnel was built mainly for studying the spinning characteristics of airplane models, but may be used as well for the usual types of wind-tunnel tests. A special spinning balance is being developed to measure the desired forces and moments with the model simulating the spin of an airplane. Satisfactory air flow has been attained with a velocity that is uniform over the jet to within plus or minus 0.5 per cent. The turbulence present in the tunnel has been compared with that of several other tunnels by means of the results of sphere drag tests and was found to average well with the values of those tunnels. Included also in the report are comparisons of results of stable autorotation and of rolling-moment test obtained both in the vertical tunnel and in the old horizontal 5-foot atmospheric tunnel. (author)
Document ID
19930091086
Document Type
Other
Authors
Wenzinger, Carl J
Harris, Thomas A
Date Acquired
September 6, 2013
Publication Date
January 1, 1931
Report/Patent Number
NACA-TR-387
Accession Number
93R20376
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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