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Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of the NACA 653-418, A=1.0 Airfoil Section
Document ID
19930092798
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Quinn, John H , Jr
Date Acquired
September 6, 2013
Publication Date
November 1, 1945
Report/Patent Number
NACA-WR-L-82
NACA-CB-L5J04
Report Number: NACA-WR-L-82
Report Number: NACA-CB-L5J04
Accession Number
93R22088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS-NACA-LOW-TURBULENCE (LMAL)
WIND TUNNEL TESTS-NACA-PRESSURE, TWO-DIMENSIONAL(LMAL) (7 1/2' X 3')
REYNOLDS NUMBER
AIRFOILS-CHARACTERISTICS EFFECT OF SURFACE ROUGHNESS
AIRFOILS-NACA 653-418-LOW-DRAG CHARACTERISTICS

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