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Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effectsThis report documents an analytical study of the response of unsymmetrically laminated cylinders subjected to thermally-induced preloading effects and compressive axial load. Closed-form solutions are obtained for the displacements and intralaminar stresses and recursive relations for the interlaminar shear stress were obtained using the closed-form intralaminar stress solutions. For the cylinder geometries and stacking sequence examples analyzed, several important and as yet undocumented effects of including thermally-induced preloading in the analysis are observed. It should be noted that this work is easily extended to include uniform internal and/or external pressure loadings and the application of strain and stress failure theories.
Document ID
19930015723
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Paraska, Peter J.
(Naval Surface Warfare Center Bethesda, MD, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-192788
CARDEROCKDIV-U-SSM-65-93/03
NAS 1.26:192788
Report Number: NASA-CR-192788
Report Number: CARDEROCKDIV-U-SSM-65-93/03
Report Number: NAS 1.26:192788
Accession Number
93N24912
Funding Number(s)
CONTRACT_GRANT: NAG1-901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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