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Theoretical analysis of oscillations in hovering of helicopter blades with inclined and offset flapping and lagging hinge axes
Document ID
19930082876
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Morduchow, M (Polytechnic Institute of Brooklyn)
Hinchey, F G (Polytechnic Institute of Brooklyn)
Date Acquired
August 16, 2013
Publication Date
December 1, 1950
Report/Patent Number
NACA-TN-2226
Report Number: NACA-TN-2226
Accession Number
93R12166
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTOR BLADES - FLAPPING
ROTOR BLADES, HINGED
ROTOR BLADES - OSCILLATIONS
ROTOR BLADES - STABILITY
PROPELLERS, HELICOPTER

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