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Hovering performance characteristics of a rotor with and without blade-pitch servo-control flapsPhotographic performance evaluation of hovering helicopter rotor with and without blade pitch servocontrol flaps
Document ID
19670006629
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Shivers, J. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3786
Report Number: NASA-TN-D-3786
Accession Number
67N15958
Funding Number(s)
CONTRACT_GRANT: 721-01-00-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HELICOPTER ROTOR
PERFORMANCE CHARACTERISTICS
HOVERING STABILITY

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