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Improvement of analytical dynamic models using modal test dataA method developed to determine maximum changes in analytical mass and stiffness matrices to make them consistent with a set of measured normal modes and natural frequencies is presented. The corrected model will be an improved base for studies of physical changes, boundary condition changes, and for prediction of forced responses. The method features efficient procedures not requiring solutions of the eigenvalue problem, and the ability to have more degrees of freedom than the test data. In addition, modal displacements are obtained for all analytical degrees of freedom, and the frequency dependence of the coordinate transformations is properly treated.
Document ID
19800050912
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Berman, A.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Wei, F. S.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Rao, K. V.
(Kaman Aerospace Corp. Bloomfield, Conn., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 80-0800
Meeting Information
Meeting: Structures, Structural Dynamics, and Materials Conference
Location: Seattle, WA
Start Date: May 12, 1980
End Date: May 14, 1980
Accession Number
80A35082
Funding Number(s)
CONTRACT_GRANT: NAS1-15805
Distribution Limits
Public
Copyright
Other

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