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Wide range stress intensity factor expressions for ASTM E 399 standard fracture toughness specimensFor each of the two types of specimens, bend and compact, described previously for plane strain fracture toughness of materials, E 399, a polynominal expression is given for calculation of the stress intensity factor, K, from the applied force, P, and the specimen dimensions. It is explicitly stated, however, that these expressions should not be used outside the range of relative crack length, a/W, from 0.45 to 0.55. While this range is sufficient for the purpose of E 399, the same specimen types are often used for other purposes over a much wider range of a/W; for example, in the study of fatigue crack growth. Expressions are presented which are at least as accurate as those in E 399-74, and which cover much wider ranges of a/W: for the three-point bend specimen from 0 to 1; and for the compact specimen from 0.2 to 1. The range has to be restricted for the compact specimen because of the proximity of the loading pin holes to the crackline, which causes the stress intensity factor to be sensitive to small variations in dimensions when a/W is small. This is a penalty inherently associated with the compactness of the specimen.
Document ID
19760012381
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srawley, J. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Structural Mechanics
Report/Patent Number
E-8654
NASA-TM-X-71881
Report Number: E-8654
Report Number: NASA-TM-X-71881
Meeting Information
Meeting: Conf. of Am. Soc. for Testing and Mater., Committee E-24
Location: Orlando, FL
Country: United States
Start Date: March 22, 1976
End Date: March 26, 1976
Accession Number
76N19469
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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