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Nonlinear random response prediction using MSC/NASTRANAn equivalent linearization technique was incorporated into MSC/NASTRAN to predict the nonlinear random response of structures by means of Direct Matrix Abstract Programming (DMAP) modifications and inclusion of the nonlinear differential stiffness module inside the iteration loop. An iterative process was used to determine the rms displacements. Numerical results obtained for validation on simple plates and beams are in good agreement with existing solutions in both the linear and linearized regions. The versatility of the implementation will enable the analyst to determine the nonlinear random responses for complex structures under combined loads. The thermo-acoustic response of a hexagonal thermal protection system panel is used to highlight some of the features of the program.
Document ID
19940013177
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Robinson, J. H.
(NASA Langley Research Center Hampton, VA, United States)
Chiang, C. K.
(Old Dominion Univ. Hampton, VA., United States)
Rizzi, S. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1993
Subject Category
Acoustics
Report/Patent Number
NAS 1.15:109029
NASA-TM-109029
Report Number: NAS 1.15:109029
Report Number: NASA-TM-109029
Accession Number
94N17650
Funding Number(s)
PROJECT: RTOP 505-63-50-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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