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Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of Three Airfoil Sections Formed by Cutting off Various Amounts from the Rear Portion of the NACA 0012 Airfoil Section
Document ID
19930082748
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Smith, Hamilton A
Schaefer, Raymond F
Date Acquired
August 16, 2013
Publication Date
April 1, 1950
Report/Patent Number
NACA-TN-2074
Accession Number
93R12038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - CHARACTERISTICS - EFFECT OF SURFACE ROUGHNESS
WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE
AIRFOILS - NACA 0012 - CHAR , A C , MOMENTS & ORDINATES - HELICOPTER
AIRFOILS - CHARACTERISTICS - EFFECT OF RIVET HEADS
AIRFOILS - CHARACTERISTICS -EFFECT OF TRAILING-EDGE SHAPE

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