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Fracture mechanics correlation of boron/aluminum coupons containing stress risersThe mechanical behavior of boron/aluminum near stress risers has been studied and reported. This effort was directed toward defining the tensile behavior of both unidirectional and (0/ plus or minus 45) boron/aluminum using linear elastic fracture mechanics (LEFM). The material used was 5.6-mil boron in 6061 aluminum, consolidated using conventional diffusion bonding techniques. Mechanical properties are reported for both unidirectional and (0/ plus or minus 45) boron/aluminum, which serve as control data for the fracture mechanics predictions. Three different flawed specimen types were studied. In each case the series of specimens remained geometrically similar to eliminate variations in finite size correction factors. The fracture data from these tests were reduced using two techniques. They both used conventional LEFM methods, but the existence of a characteristic flaw was assumed in one case and not the other. Both the data and the physical behavior of the specimens support the characteristic flaw hypothesis. Cracks were observed growing slowly in the (0/ plus or minus 45) laminates, until a critical crack length was reached at which time catastrophic failure occurred.
Document ID
19760033855
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Adsit, N. R.
(General Dynamics Corp. San Diego, CA, United States)
Waszczak, J. P.
(General Dynamics Corp. Convair Div., San Diego, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Composite Materials
Meeting Information
Meeting: Fracture mechanics of composites
Location: Gaithersburg, MD
Start Date: September 25, 1974
Accession Number
76A16821
Distribution Limits
Public
Copyright
Other

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