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Comparison of Flight Measured Helicopter Rotor Blade Chordwise Pressure Distributions and Two-Dimensional Airfoil CharacteristicsHelicopter rotor blade chordwise pressure distribution and two-dimensional airfoil characteristics
Document ID
19630011950
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kelley, H. L. (NASA Langley Research Center Hampton, VA, United States)
Scheiman, J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1963
Subject Category
Biosciences
Accession Number
63N21830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTOR BLADE
HELICOPTER ROTOR
AIRFOIL CHARACTERISTICS
PRESSURE DISTRIBUTION

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