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The Effects at Transonic Speeds of Thickening the Trailing Edge of a Wing with a 4-percent-thick Circular-arc Airfoil
Document ID
19930087063
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cleary, Joseph W
Stevens, George L
Date Acquired
August 16, 2013
Publication Date
December 11, 1951
Report/Patent Number
NACA-RM-A51J11
Accession Number
93R16353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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