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Cmparison of flight-measured helicopter rotor-blade chordwise pressure distributions with static two-dimensional airfoil characteristicsHelicopter rotor blade pressure distributions compared with static two-dimensional airfoil characteristics for extreme flight conditions
Document ID
19670014489
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
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
May 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3936
Report Number: NASA-TN-D-3936
Accession Number
67N23818
Funding Number(s)
CONTRACT_GRANT: 721-01-00-29-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOIL CHARACTERISTICS
PRESSURE DISTRIBUTION
HELICOPTER
ROTOR BLADE
FLIGHT CONDITION

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