Residual flexibility test method for verification of constrained structural modelsA 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.
Document ID
19920051814
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
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 15, 2013
Publication Date
January 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-2325Report Number: AIAA PAPER 92-2325
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference