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Automated dynamic analytical model improvementA method is developed and illustrated which finds minimum changes in analytical mass and stiffness matrices to make them consistent with a set of measured normal modes and natural frequencies. The corrected model is an improved base for studies of physical changes, changes in boundary conditions, and for prediction of forced responses. Features of the method are: efficient procedures not requiring solutions of the eigenproblem; the model may have more degrees of freedom than the test data; modal displacements at all the analytical degrees of freedom are obtained; the frequency dependence of the coordinate transformations are properly treated.
Document ID
19810020924
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Berman, A.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-3452
R-1624
Accession Number
81N29462
Funding Number(s)
CONTRACT_GRANT: NAS1-15805
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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