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Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheetStress-intensity factors are determined for a cracked infinite sheet adhesively bonded to a stringer, and debonding of the adhesive layer is predicted. The stringer is modeled as a semi-infinite sheet. Adhesive nonlinearity is also included. Both the sheet and stringer are treated as homogeneous, orthotropic materials. A set of integral equations is formulated and solved to obtain the adhesive shear stresses and crack-tip stress-intensity factors. Adhesive debonding is predicted using a rupture criterion based on the combined adhesive stresses. When the crack is not under the stringer, the debond extends along the edge of the stringer. When the crack tip is beneath the stringer, the debond grows to the end of the crack, then along the edge of the stringer. Stress levels required for debond initiation decrease as the crack tip is moved beneath the stringer. With a nonlinear adhesive, the debond initiates at higher applied stress levels than in linear adhesive cases. Compared with the linear adhesive solution, modeling a nonlinear adhesive causes the stress-intensity factor to increase when the bond is assumed to remain intact but causes the stress-intensity factor to decrease when debonding is included.
Document ID
19860007144
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bigelow, C. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-87598
NAS 1.15:87598
L-16027
Report Number: NASA-TM-87598
Report Number: NAS 1.15:87598
Report Number: L-16027
Accession Number
86N16614
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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