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Fracture analysis of various cracked configurations in sheet and plate materialsA two-parameter fracture criterion was derived which relates the linear-elastic stress-intensity factor at failure, the elastic nominal failure stress, and two material parameters. The fracture criterion was used previously to analyze fracture data for surface- and through-cracked sheet and plate specimens under tensile loading. The fracture criterion was applied to center-crack tension, compact, and notch-band fracture specimens made of steel, titanium, or aluminum alloy materials tested at room temperature. The fracture data included a wide range of crack lengths, specimen widths, and thicknesses. The materials analyzed had a wide range of tensile properties. Failure stresses calculated using the criterion agreed well (plus or minus 10 percent) with experimental failure stresses. The criterion was also found to correlate fracture data from different specimen types (such as center-crack tension and compact specimens), within plus or minus 10 percent for the same material, thickness, and test temperature.
Document ID
19750019342
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-72709
Report Number: NASA-TM-X-72709
Meeting Information
Meeting: ASTM Symp. on Properties Related to Toughness
Location: Montreal
Country: Canada
Start Date: July 23, 1975
End Date: July 27, 1975
Accession Number
75N27414
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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