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The Comparison of Well-known and New Wing Sections Tested in the Variable Density Wind TunnelThree groups of airfoils have been tested in the variable density wind tunnel. The first group contains three airfoils. The second group is a systematic series of twenty-seven airfoils. The third group consists of several frequently used wing sections.
Document ID
19930081027
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Higgins, George J
Date Acquired
September 6, 2013
Publication Date
May 1, 1925
Report/Patent Number
NACA-TN-219
Report Number: NACA-TN-219
Accession Number
93R10317
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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