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Integrating-matrix method for determining the natural vibration characteristics of propeller bladesIntegrating matrix method for determining natural lateral vibration data on rotating twisted propeller blade
Document ID
19710003548
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hunter, W. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1970
Subject Category
Structural Mechanics
Report/Patent Number
L-5539
NASA-TN-D-6064
Report Number: L-5539
Report Number: NASA-TN-D-6064
Accession Number
71N13023
Funding Number(s)
CONTRACT_GRANT: 721-01-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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