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A thermoelastic transversely isotropic thick walled cylinder/disk application: An analytical solution and studyA continuum theory is utilized to represent the thermoelastic behavior of a thick walled composite cylinder that can be idealized as transversely isotropic. A multiaxial statement of the constitutive theory employed is presented, as well as the out of the plane of isotropy, plane stress, and plane strain reductions. The derived analytical solution presented is valid for a cylindrical tube or thin disk with a concentric hole, subjected to internal and/or external pressure and a general radial temperature distribution. A specific problem examined is that of a thick walled cylinder subjected to an internal and external pressure loading and a linear radial temperature distribution. The results are expressed in nondimensional form and the effects on the response behavior are examined for various material properties, fiber orientation and types of loadings.
Document ID
19900003634
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Arnold, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1989
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-102320
NAS 1.15:102320
E-5016
Accession Number
90N12950
Funding Number(s)
PROJECT: RTOP 510-01-0A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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