NASA NTRS · 19920051814
Residual flexibility test method for verification of constrained structural models
Abstract
A method is presented for deriving constrained modes and frequencies from a model correlated to a set of free-free test modes and a set of measured residual flexibilities. The method involves a simple modification of the MacNeal and Rubin component mode representation to allow verification of a constrained structural model. Results for two spaceflight structures show quick convergence of constrained modes using an easily measurable set of free-free modes plus the residual flexibility matrix or its boundary partition. This paper further validates the residual flexibility approach as an alternative test/analysis method when fixed-base testing proves impractical.
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Admire, John R., Tinker, Michael L., Ivey, Edward W.. 1992-01-01. Residual flexibility test method for verification of constrained structural models. https://ntrs.nasa.gov/citations/19920051814
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