Estimating the Statistical Properties of Crack Growth for Small Cracks

Item

Title
Estimating the Statistical Properties of Crack Growth for Small Cracks
Date
1980
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AFWAL TR 81-4016
Creator
Hovey, P. W.
Gallagher, J. P.
Berens, A. P.
Corporate Author
University of Dayton Research Institute
Extent
26
Identifier
ADA104672
Distribution Classification
1
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
A series of statistical studies were conducted on two sets of fatigue crack growth data which were generated under variable amplitude loading from cracks that initiated in 7475-T7351 Aluminum down in the bore of typical aircraft quality prepared holes. The study considered fatigue crack growth (life) behavior and fatigue crack growth rate behavior. Generally, the study showed that small crack growth behavior was similar to that observed for larger cracks and that a stress intensity factor parameter could be used to describe the mean trend of the fatigue crack growth rate behavior via a power law relationship.
Report Availability
Full text available by request
Date Issued
1980-12-01
Provenance
IIT
Type
report
Format
26 pages ; 28 cm.

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