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Second order non-linear equations of motion for spinning highly flexible line elementsThe second order nonlinear equations of motion are formulated for spinning line elements having little or no intrinsic structural stiffness. The derivation is based on the extended Hamilton's principle and includes the effect of initial geometric imperfections (axial, curvature, and twist) on the line element dynamics. For comparison with previous work, the nonlinear equations are reduced to a linearized form frequently found in the literature. The comparison revealed several new spin-stiffening terms that have not been previously identified and/or retained. They combine geometric imperfections, rotary inertia, Coriolis, and gyroscopic terms.
Document ID
19820042782
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Salama, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Trubert, M.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Essawi, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Utku, S.
(Duke University Durham, NC, United States)
Date Acquired
August 10, 2013
Publication Date
February 22, 1982
Publication Information
Publication: Journal of Sound and Vibration
Volume: 80
Subject Category
Physics (General)
Accession Number
82A26317
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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