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Simplified data reduction methods for the ECT test for mode 3 interlaminar fracture toughnessSimplified expressions for the parameter controlling the load point compliance and strain energy release rate were obtained for the Edge Crack Torsion (ECT) specimen for mode 3 interlaminar fracture toughness. Data reduction methods for mode 3 toughness based on the present analysis are proposed. The effect of the transverse shear modulus, G(sub 23), on mode 3 interlaminar fracture toughness characterization was evaluated. Parameters influenced by the transverse shear modulus were identified. Analytical results indicate that a higher value of G(sub 23) results in a low load point compliance and lower mode 3 toughness estimation. The effect of G(sub 23) on the mode 3 toughness using the ECT specimen is negligible when an appropriate initial delamination length is chosen. A conservative estimation of mode 3 toughness can be obtained by assuming G(sub 23) = G(sub 12) for any initial delamination length.
Document ID
19950023404
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Li, Jian
(NASA Langley Research Center Hampton, VA, United States)
Obrien, T. Kevin
(Army Research Lab. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-110176
ARL-MR-234
NAS 1.15:110176
Report Number: NASA-TM-110176
Report Number: ARL-MR-234
Report Number: NAS 1.15:110176
Accession Number
95N29825
Funding Number(s)
PROJECT: RTOP 505-63-50-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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