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Residual flexibility test method for verification of constrained structural modelsA method is described for deriving constrained modes and frequencies from a reduced model based on a subset of the free-free modes plus the residual effects of neglected modes. The method involves a simple modification of the MacNeal and Rubin component mode representation to allow development of a verified constrained (fixed-base) structural model. Results for two spaceflight structures having translational boundary degrees of freedom show quick convergence of constrained modes using a measureable number of free-free modes plus the boundary partition of the residual flexibility matrix. This paper presents the free-free residual flexibility approach as an alternative test/analysis method when fixed-base testing proves impractical.
Document ID
19950055989
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Admire, John R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Tinker, Michael L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Ivey, Edward W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1994
Publication Information
Publication: AIAA Journal
Volume: 32
Issue: 1
ISSN: 0001-1452
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
95A87588
Funding Number(s)
CONTRACT_GRANT: NAS8-38251
Distribution Limits
Public
Copyright
Other

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