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A cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheetThe stress intensity factor is determined for a cracked orthotropic sheet adhesively bonded to an orthotropic stringer. Since the stringer is modeled as a semiinfinite sheet, the solution is most appropriate for a crack tip located near a stringer edge. Both adherends are treated as homogeneous, orthotropic media. It is assumed they are in plane stress and the adhesive is in pure shear. From Green's functions and the complex variable theory of orthotropic elasticity developed by Lekhnitskiy, a set of integral equations is obtained. The integral equations are replaced by an equivalent set of algebraic equations which is solved to obtain the shear stress distribution in the adhesive layer. With these stresses, equations for the stress intensity factors at both crack tips are found. A parametric study is conducted to determine the sensitivity of the system to material properties and specimen configuration. Unless the crack tip is very close to or under the stringer the stress intensity factor is approximately that of an unstiffened sheet. However, as the crack propagates beneath the stringer, the stress intensity factor decreases significantly. Increasing the stiffness of the stringer or the adhesive also results in a decrease in the stress intensity factor.
Document ID
19850024026
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Bigelow, C. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1985
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TP-2455
NAS 1.60:2455
L-15972
Report Number: NASA-TP-2455
Report Number: NAS 1.60:2455
Report Number: L-15972
Accession Number
85N32339
Funding Number(s)
PROJECT: RTOP 506-53-23-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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