NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Short fatigue cracks in notched aluminum specimensThe short-crack fatigue behavior in notched specimens of Al 2024-T3 was studied at values of the stress ratio, R, equal to 0.5, 0.0, -1.0, and -2.0. Crack growth was monitored using a replica technique for cracks ranging in length from a few tens of a micron to the specimen's thickness (2.3 mm). Crack opening displacement was measured for surface cracks as short as 0.035 mm using the interferometric strain/displacement gage, a laser-based optical technique described by Sharpe (1982). It was found that the growth rates of short cracks were faster than the rates of long cracks for R values of -1.0 and -2.0. No significant difference was observed for R = 0.0, and at R = 0.5, the short cracks actually grew more slowly that the long ones. At all R values, the closure stresses measured for short cracks were smaller than those predicted for large cracks.
Document ID
19870047390
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, J. J.
(Johns Hopkins Univ. Baltimore, MD, United States)
Sharpe, W. N., Jr.
(Johns Hopkins University Baltimore, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Metallic Materials
Accession Number
87A34664
Funding Number(s)
CONTRACT_GRANT: NAG1-526
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available