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Vibratory hub load data reduction and analysis from the reverse velocity rotor wind tunnel test, phase 2BThe vibratory hub loads data analysis from the reverse velocity rotor wind tunnel test is reported. Vibratory loads were obtained from the rotating hub balance and also by synthesis of generalized coordinates from the blade flap bending moments. Load trends were defined as a function of speed, rotor thrust and 2 per rev cyclic from each of the data methods. These trends were compared to determine the degree of agreement between each method and provide substantiation for the generalized coordinate approach.
Document ID
19760008950
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Taylor, R. B.
(Boeing Vertol Co. Philadelphia, PA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-137780
D210-11004-1
Report Number: NASA-CR-137780
Report Number: D210-11004-1
Accession Number
76N16038
Funding Number(s)
CONTRACT_GRANT: NAS2-8630
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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