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Predicting failure of specimens with either surface cracks or corner cracks at holesA previously developed fracture criterion was applied to fracture data for surface-cracked specimens subjected to remote tensile loading and for specimens with a corner crack (or cracks) emanating from a circular hole subjected to either remote tensile loading or pin loading in the hole. The failure stresses calculated from this criterion were consistent with experimental failure stresses for both surface and corner cracks for a wide range of crack shapes and crack sizes in specimens of aluminum alloy, titanium alloy, and steel. Empirical equations for the elastic stress-intensity factors for a surface crack and for a corner crack (or cracks) emanating from a circular hole in a finite-thickness and finite-width specimen were also developed.
Document ID
19760019499
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-8244
L-10203
Report Number: NASA-TN-D-8244
Report Number: L-10203
Accession Number
76N26587
Funding Number(s)
PROJECT: RTOP 505-02-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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