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Short fatigue crack behavior in notched 2024-T3 aluminum specimensSingle-edge, semi-circular notched specimens of Al 2024-T3, 2.3 mm thick, were cyclicly loaded at R-ratios of 0.5, 0.0, -1.0, and -2.0. The notch roots were periodically inspected using a replica technique which duplicates the bore surface. The replicas were examined under an optical microscope to determine the initiation of very short cracks and to monitor the growth of short cracks ranging in length from a few tens of microns to the specimen thickness. In addition to short crack growth measurements, the crack opening displacement (COD) was measured for surface cracks as short as 0.035 mm and for through-thickness cracks using the Interferometric Strain/Displacement Gage (ISDG), a laser-based optical technique. The growth rates of short cracks were faster than the long crack growth rates for R-ratios of -1.0 and -2.0. No significant difference between short and long crack growth rates was observed for R = 0.0. Short cracks had slower growth rates than long cracks for R = 0.5. The crack opening stresses measured for short cracks were smaller than those predicted for large cracks, with little difference appearing for positive R-ratios and large differences noted for negative R-ratios.
Document ID
19870016931
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, J. J.
(Johns Hopkins Univ. Baltimore, MD, United States)
Sharpe, W. N., Jr.
(Johns Hopkins Univ. Baltimore, MD, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:180314
NASA-CR-180314
Report Number: NAS 1.26:180314
Report Number: NASA-CR-180314
Accession Number
87N26364
Funding Number(s)
CONTRACT_GRANT: NAG1-526
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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