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Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios
Document ID
19930092777
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tetervin, Neal
Date Acquired
September 6, 2013
Publication Date
September 1, 1943
Report/Patent Number
NACA-CB-3I13
NACA-WR-L-452
Report Number: NACA-CB-3I13
Report Number: NACA-WR-L-452
Accession Number
93R22067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION-AIRFOILS-NACA HELICOPTER
PITCHING MOMENTS-AIRFOILS-NACA
REYNOLDS NUMBER
LIFT & DRAG RATIO
WINGS, ROTATING
AIRFOIL SURFACES-ROUGHNESS
DRAG, PROFILE
AIRFOILS-ROTOR BLADES
MACH NUMBER
AIRFOILS-NACA 23015-CHAR , A C , MOMENTS & ORDINATES

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