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Investigation of the Variation of Lift Coefficient with Reynolds Number at a Moderate Angle of Attack on a Low-Drag Airfoil
Document ID
19930092736
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tetervin, Neal
Date Acquired
September 6, 2013
Publication Date
January 1, 1942
Report/Patent Number
NACA-WR-L-661
Report Number: NACA-WR-L-661
Accession Number
93R22026
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - ANGLE OF ATTACK
BOUNDARY LAYER SEPARATION - AIRFOILS
REYNOLDS NUMBER
BOUNDARY LAYER - VELOCITY DISTRIBUTION
WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2' X 3')
LIFT COEFFICIENTS - AIRFOILS
PHOTOGRAPHY - AIR FLOW - AIRFOILS LAMPBLACK
PRESSURE DISTRIBUTION - AIRFOILS - NACA 66,2-216
AIRFOILS - NACA 66,2-216 - CHARACTERISTICS LOW-DRAG

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