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A finite element analysis of fatigue crack closureExperiments have shown that fatigue cracks close at positive loads during constant-amplitude load cycling. The crack-closure phenomenon is caused by residual plastic deformations remaining in the wake of an advancing crack tip. The present paper is concerned with the application of a two-dimensional, nonlinear, finite-element analysis for predicting crack-closure and crack-opening stresses during cyclic loading. A two-dimensional finite-element computer program, which accounts for both elastic-plastic material behavior and changing boundary conditions associated with crack extension and intermittent contact of the crack surfaces under cyclic loading, has been developed. An efficient technique to account for changing boundary conditions was also incorporated into the nonlinear analysis program. This program was subsequently used to study crack extension and crack closure under constant-amplitude and two-level block loading. The calculated crack-closure and crack-opening stresses were qualitatively consistent with experimental observations.
Document ID
19740024240
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
L-9715
NASA-TM-X-72005
Report Number: L-9715
Report Number: NASA-TM-X-72005
Meeting Information
Meeting: Natl. Symp. on Fracture Mech.
Location: Providence
Start Date: August 26, 1974
End Date: August 28, 1974
Accession Number
74N32353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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