NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The crack problem in a reinforced cylindrical shellIn this paper a partially reinforced cylinder containing an axial through crack is considered. The reinforcement is assumed to be fully bonded to the main cylinder. The composite cylinder is thus modelled by a nonhomogeneous shell having a step change in the elastic properties at the z=0 plane, z being the axial coordinate. Using a Reissner type transverse shear theory the problem is reduced to a pair of singular integral equations. In the special case of a crack tip touching the bimaterial interface it is shown that the dominant parts of the kernels of the integral equations associated with both membrane loading and bending of the shell reduce to the generalized Cauchy kernel obtained for the corresponding plane stress case. The integral equations are solved and the stress intensity factors are given for various crack and shell dimensions. A bonded fiberglass reinforcement which may serve as a crack arrestor is used as an example.
Document ID
19860017176
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yahsi, O. S.
(Middle East Technical Univ. Ankara, Turkey)
Erdogan, F.
(Lehigh Univ. Bethlehem, PA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:176686
NASA-CR-176686
Report Number: NAS 1.26:176686
Report Number: NASA-CR-176686
Accession Number
86N26648
Funding Number(s)
CONTRACT_GRANT: NGR39-007-011
CONTRACT_GRANT: NSF MEA-84-14477
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available