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Sizing Single Cantilever Beam Specimens for Characterizing Facesheet/Core Peel Debonding in Sandwich StructureThis technical publication details part of an effort focused on the development of a standardized facesheet/core peel debonding test procedure. The purpose of the test is to characterize facesheet/core peel in sandwich structure, accomplished through the measurement of the critical strain energy release rate associated with the debonding process. Following an examination of previously developed tests and a recent evaluation of a selection of these methods, a single cantilever beam (SCB) specimen was identified as being a promising candidate for establishing such a standardized test procedure. The objective of the work described here was to begin development of a protocol for conducting a SCB test that will render the procedure suitable for standardization. To this end, a sizing methodology was developed to ensure appropriate SCB specimen dimensions are selected for a given sandwich system. Application of this method to actual sandwich systems yielded SCB specimen dimensions that would be practical for use. This study resulted in the development of a practical SCB specimen sizing method, which should be well-suited for incorporation into a standardized testing protocol.
Document ID
20100003052
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Ratcliffe, James G.
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Subject Category
Composite Materials
Report/Patent Number
LF99-10031
NASA/TP-2010-216169
L-19806
Funding Number(s)
WBS: WBS 814358.02.01.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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