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Finite element models of wire rope for vibration analysisThe usefulness of wire rope in shock and vibration isolation is briefly reviewed and its modeling for the purpose of vibration analysis is addressed. A model of a nominally straight segment of wire rope is described in which the rope structure is represented by a maiden, or central, strand of wire with one (or more) strand(s) wrapped around it in a helix (helices). The individual strands are modeled using finite elements and MSC NASTRAN. Small linear segments of each wire are modeled mathematically by dividing them lengthwise into triangular prisms representing each prism by a solid NASTRAN element. To model pretensioning and allow for extraction of internal force information from the NASTRAN model, the wound strands are connected to the maiden strand and each other using spring (scalar elastic) elements. Mode shapes for a length of wire rope with one and fixed to a moving base and the other attached to a point mass, are presented. The use of the NASTRAN derived mode shapes to approximate internal normal forces in equations of motion for vibration analyses is considered.
Document ID
19870013315
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cochran, J. E., Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Fitz-Coy, N. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Cutchins, M. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Structural Mechanics
Accession Number
87N22748
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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