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Experimental investigation of flutter of a propeller with Clark Y section operating at zero forward velocity at positive and negative blade- angle settings
Document ID
19930082622
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Baker, John E
Paulnock, Russell S
Date Acquired
August 16, 2013
Publication Date
December 1, 1949
Report/Patent Number
NACA-TN-1966
Accession Number
93R11912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - LAL - SPHERES, SUPERSONIC
FLUTTER - PROPELLERS
PROPELLERS - STALLING
PROPELLERS - CHARACTERISTICS
PROPELLER BLADES - SETTING
AIRFOILS - CLARK Y - CHARACTERISTICS PROPELLER

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