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The Use of Doublers in Delamination Toughness TestingIn this paper, the data reduction equations for common delamination toughness tests are rederived for use with specimens which have bonded doublers. The common toughness tests considered here are the double cantilever beam (DCB) for mode I toughness; the end notch flexure (3ENF) and 4 point ENF (4ENF) for mode II toughness; and the mixed mode bending (MMB) test for testing under combined mode I and mode II loading. Because the addition of the doublers changes the bending stiffness of the specimens, these data reduction equations may need to be corrected. Doublers were added to the delamination test specimens to solve a premature failure problem. Delamination toughness is normally tested using a beam with an imbedded insert so that one end of the specimen is split into two arms. If the specimen is too thin, or if the toughness of the material is too high, an arm of the specimen may fail in bending before the delamination grows. When this occurs, the toughness of the material cannot be determined. To delay the bending failure so that delamination growth occurs, doubler plates were bonded to both top and bottom surfaces of the specimen. A doubler parameter, beta, which describes how much the use of doubler plates changed the ratio of full thickness to delaminated bending stiffnesses, was defined. When changes to the data reduction equations were required, the changes were minor when written in terms of the beta parameter. The doubler plate technique was demonstrated by measuring the mixed-mode fracture toughness of a carbon-carbon composite using test specimens which would otherwise have failed before delamination growth occurred. The doubler plate technique may solve several problems that can be encountered when testing delamination fracture toughness.
Document ID
20030015408
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Reeder, James R.
(NASA Langley Research Center Hampton, VA United States)
Demarco, Kevin
(Swales Aerospace Hampton, VA United States)
Whitley, Karen S.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Quality Assurance And Reliability
Meeting Information
Meeting: American Society for Composites 17th Technical Conference
Location: West Lafayette, IN
Country: United States
Start Date: October 21, 2002
End Date: October 23, 2002
Sponsors: American Society for Composites
Distribution Limits
Public
Copyright
Public Use Permitted.
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