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Tests in the Variable Density Wind Tunnel to Investigate the Effects of Scale and Turbulence on Airfoil CharacteristicsThe effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 0021, the Clark Y and the USA 35-A, and the USN PS6, have been investigated in the Variable Density Wind Tunnel of the NACA. Tests were made over a wide scale range for only two different conditions of turbulence.
Document ID
19930081155
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stack, John
Date Acquired
September 6, 2013
Publication Date
February 1, 1931
Report/Patent Number
NACA-TN-364
Accession Number
93R10445
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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