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Nonlinear vibration and stability of rotating, pretwisted, preconed blades including Coriolis effectsThe coupled bending-bending-torsional equations of dynamic motion of rotating, linearly pretwisted blades are derived including large precone, second degree geometric nonlinearities and Coriolis effects. The equations are solved by the Galerkin method and a linear perturbation technique. Accuracy of the present method is verified by conparisons of predicted frequencies and steady state deflections with those from MSC/NASTRAN and from experiments. Parametric results are generated to establish where inclusion of only the second degree geometric nonlinearities is adequate. The nonlinear terms causing torsional divergence in thin blades are identified. The effects of Coriolis terms and several other structurally nonlinear terms are studied, and their relative importance is examined.
Document ID
19870052622
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Subrahmanyam, K. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Kaza, K. R. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Brown, G. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Lawrence, C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
May 1, 1987
Publication Information
Publication: Journal of Aircraft
Volume: 24
ISSN: 0021-8669
Subject Category
Structural Mechanics
Accession Number
87A39896
Distribution Limits
Public
Copyright
Other

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