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Theoretical Investigation of Thermo-Mechanical Behavior of Carbon Nanotube-Based Composites Using the Integral Transform MethodThis project uses the integral transform technique to model the problem of nanotube behavior as an axially symmetric system of shells. Assuming that the nanotube behavior can be described by the equations of elasticity, we seek a stress function x which satisfies the biharmonic equation: del(exp 4) chi = [partial deriv(r(exp 2)) + partial deriv(r) + partial deriv(z(exp 2))] chi = 0. The method of integral transformations is used to transform the differential equation. The symmetry with respect to the z-axis indicates that we only need to consider the sine transform of the stress function: X(bar)(r,zeta) = integral(from 0 to infinity) chi(r,z)sin(zeta,z) dz.
Document ID
20020040125
Acquisition Source
Goddard Space Flight Center
Document Type
Other
Authors
Pawloski, Janice S.
(Hope Coll. Holland, MI United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Subject Category
Composite Materials
Report/Patent Number
NLPN-01-0022
NRA-99-05-OSS-0897
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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