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Finite element thermal-structural analysis of cable-stiffened space structuesFinite element thermal-structural analyses of large, cable-stiffened space structures are presented. A computational scheme for the calculation of prestresses in the cable-stiffened structures is also described. The determination of thermal loads on orbiting space structures due to environment heating is discussed briefly. Three finite element structural analysis techniques are presented for the analysis of prestressed structures. Linear, stress stiffening, and large displacement analysis techniques were investigated. These three techniques were employed for analysis of prestressed cable structures at different prestress levels. The analyses produced similar results at small prestress, but at higher prestress, differences between the results became significant. For the cable-stiffened structures studied, the linear analysis technique may not provide acceptable results. The stress stiffening analysis technique may yield results of acceptable accuracy depending upon the level of prestress. The large displacement analysis technique produced accurate results over a wide range of prestress and is recommended as a general analysis technique for thermal-structural analysis of cable-stiffened space structures.
Document ID
19840020039
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thornton, E. A.
(Old Dominion Univ. Norfolk, VA, United States)
Dechaumphai, P.
(Old Dominion Univ. Norfolk, VA, United States)
Pandey, A. K.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1984
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:173709
NASA-CR-173709
Report Number: NAS 1.26:173709
Report Number: NASA-CR-173709
Accession Number
84N28108
Funding Number(s)
CONTRACT_GRANT: NAG1-257
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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