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Efficient reanalysis of structures by a direct modification methodA procedure for the local stiffness modifications of large structures is described. It enables structural modifications without an a priori definition of the changes in the original structure and without loss of efficiency due to multiple loading conditions. The solution procedure, implemented in NASTRAN, involved the decomposed stiffness matrix and the displacement vectors of the original structure. It solves the modified structure exactly, irrespective of the magnitude of the stiffness changes. In order to investigate the efficiency of the present procedure and to test its applicability within a design environment, several real and large structures were solved. The results of the efficiency studies indicate that the break-even point of the procedure varies between 8% and 60% stiffness modifications, depending upon the structure's characteristics and the options employed.
Document ID
19770013544
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raibstein, A. I.
(Israel Aircraft Industries Ltd. Lod, Israel)
Kalev, I.
(Israel Aircraft Industries Ltd. Lod, Israel)
Pipano, A.
(Israel Aircraft Industries Ltd. Lod, Israel)
Date Acquired
August 8, 2013
Publication Date
October 1, 1976
Publication Information
Publication: NASA. Ames Res. Center NASTRAN: User's Experiences
Subject Category
Structural Mechanics
Accession Number
77N20488
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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