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Finite element forced vibration analysis of rotating cyclic structuresA capability was added to the general purpose finite element program NASTRAN Level 17.7 to conduct forced vibration analysis of tuned cyclic structures rotating about their axes of symmetry. The effects of Coriolis and centripetal accelerations together with those due to linear acceleration of the axis of rotation were included. The theoretical development of this capability is presented.
Document ID
19840003447
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Elchuri, V.
(Textron Bell Aerospace Co. Buffalo, NY, United States)
Smith, G. C. C.
(Textron Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:165430
D2536-941008
NASA-CR-165430
Report Number: NAS 1.26:165430
Report Number: D2536-941008
Report Number: NASA-CR-165430
Accession Number
84N11515
Funding Number(s)
CONTRACT_GRANT: NAS3-22533
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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