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Multicyclic Controllable Twist Rotor Data AnalysisRsults provide functional relationship between rotor performance, blade vibratory loads and dual control settings and indicate that multicyclic control produced significant reductions in blade flatwise bending moments and blade root actuator control loads. Higher harmonic terms of servo flap deflection were found to be most pronounced in flatwise bending moment, transmission vertical vibration and pitch link vibratory load equations. The existing test hardware represents a satisfactory configuration for demonstrating MCTR technology and defining a data base for additional wind tunnel testing.
Document ID
19810009505
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wei, F. S.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Weisbrich, A. L.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Date Acquired
September 4, 2013
Publication Date
January 15, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-152251
R-1562
Report Number: NASA-CR-152251
Report Number: R-1562
Accession Number
81N18028
Funding Number(s)
CONTRACT_GRANT: NAS2-8726
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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