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Reduction of truncation errors in modal analysisA condensation method and computer program are described for large discrete parameter vibration analysis of complex structures that greatly reduces truncation errors and provides accurate definition of modes in a selected frequency range. A dynamic transformation is obtained from the partitioned equations of motion that relates modes not explicitly in the condensed solution to the retained modes at a selected system frequency. The generalized mass and stiffness matrices, obtained with existing modal synthesis methods, are reduced using this transformation and solved. Revised solutions are then obtained using new transformations at the calculated eigenvalues and are also used to assess the accuracy of the results. Computations are made tractable by simplified forms of the transformation that result with various modal synthesis methods. Three examples using the dynamic transformation in conjunction with a General Electric stiffness coupling method and the method of Craig and Bampton indicate large reductions in truncation errors and demonstrate the method for sequential groups of modes.
Document ID
19730023751
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuhar, E. J.
(General Electric Co. Philadelphia, PA, United States)
Stahle, C. V.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
September 2, 2013
Publication Date
June 29, 1973
Subject Category
Mathematics
Report/Patent Number
GE-73SD4251
NASA-CR-124446
Report Number: GE-73SD4251
Report Number: NASA-CR-124446
Accession Number
73N32484
Funding Number(s)
CONTRACT_GRANT: NAS8-28167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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