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Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps
Document ID
19930092780
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fullmer, Felicien F , Jr
Date Acquired
September 6, 2013
Publication Date
July 1, 1944
Report/Patent Number
NACA-WR-L-140
NACA-CB-L4G10
Accession Number
93R22070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS-NACA-PRESSURE, TWO-DIMENSIONAL LMAL
WING FLAPS, SPLIT
AIRFOILS-NACA 66(215)-216-CHAR , MOMENTS & ORDINATES LOW-DRAG (WING FLAPS, SPLIT
AIRFOILS-NACA 651-212-CHAR , MOMENTS & ORDINATES LOW-DRAG (WING FLAPS, SPLIT)
AIRFOILS-NACA 66,1-212-CHAR , MOMENTS & ORDINATES LOW-DRAG (WING FLAPS, SPLIT)

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