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Development of advanced modal methods for calculating transient thermal and structural responseHigher-order modal methods for predicting thermal and structural response are evaluated. More accurate methods or ones which can significantly reduce the size of complex, transient thermal and structural problems are desirable for analysis and are required for synthesis of real structures subjected to thermal and mechanical loading. A unified method is presented for deriving successively higher-order modal solutions related to previously-developed, lower-order methods such as the mode displacement and mode-acceleration methods. A new method, called the force-derivative method, is used to obtain higher-order modal solutions for both uncoupled (proportionally-damped) structural problems as well as thermal problems and coupled (non-proportionally damped) structural problems. The new method is called the force-derivative method because, analogous to the mode-acceleration method, it produces a term that depends on the forcing function and additional terms that depend on the time derivatives of the forcing function.
Document ID
19920005917
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Camarda, Charles J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:104102
NASA-TM-104102
Report Number: NAS 1.15:104102
Report Number: NASA-TM-104102
Accession Number
92N15135
Funding Number(s)
PROJECT: RTOP 506-43-71-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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