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An empirical stress-intensity factor equation for the surface crackThis paper presents an empirical stress-intensity factor equation for a surface crack as a function of parametric angle, crack depth, crack length, plate thickness and plate width for tension and bending loads. The stress-intensity factors used to develop the equation were obtained from a previous three-dimensional, finite-element analysis of semielliptical surface cracks in finite elastic plates subjected to tension or bending loads. A wide range of configuration parameters was included in the equation. The ratios of crack length to plate thickness and the ratios of crack depth to crack length ranged from 0 to 1.0. The effects of plate width on stress-intensity variations along the crack front were also included. The equation was used to predict patterns of surface-crack growth under tension or bending fatigue loads. The equation was also used to correlate surface-crack fracture data for a brittle epoxy material within + or - 10 percent for a wide range of crack shapes and crack sizes.
Document ID
19820030778
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Raju, I. S.
(NASA Langley Research Center; Joint Institute for Advancement of Flight Sciences Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Publication Information
Publication: Engineering Fracture Mechanics
Volume: 15
Issue: 1-2,
Subject Category
Structural Mechanics
Accession Number
82A14313
Distribution Limits
Public
Copyright
Other

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