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A Modified Edge Crack Torsion Test for Measurement of Mode III Fracture Toughness of Laminated Tape CompositesModifications to the edge crack torsion (ECT) test are studied to improve the reliability of this test for measuring the mode-III fracture toughness, G (sub IIIc), of laminated tape fiber-reinforced polymeric (FRP) composites. First, the data reduction methods currently used in the ECT test are evaluated and deficiencies in their accuracy are discussed. An alternative data reduction technique, which uses a polynomial form to represent ECT specimen compliance solution, is evaluated and compared to FEA (finite element analysis) results. Second, seven batches of ECT specimens are tested, each batch containing specimens with a preimplanted midplane edge delamination and midplane plies with orientations of plus theta divided by minus theta, with theta ranging from 0 degrees to 90 degrees in 15-degree increments. Tests on these specimens show that intralaminar cracking occurs in specimens from all batches except for which theta = 15 degrees and 30 degrees. Tests on specimens of these two batches are shown to result in mode-III delamination growth at the intended ply interface. The findings from this study are encouraging steps towards the use of the ECT test as a standardized method for measuring G (sub IIIc), although further modification to the data reduction method is required to make it suitable for use as part of a standardized test method.
Document ID
20160012238
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Czabaj, Michael W.
(Utah Univ. Salt Lake City, UT, United States)
Davidson, Barry D.
(Syracuse Univ. Utica, NY, United States)
Ratcliffe, James G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 11, 2016
Publication Date
September 19, 2016
Subject Category
Composite Materials
Report/Patent Number
NF1676L-25075
Paper no. 1706
Report Number: NF1676L-25075
Report Number: Paper no. 1706
Meeting Information
Meeting: American Society for Composites Technical Conference
Location: Williamsburg, VA
Country: United States
Start Date: September 19, 2016
End Date: September 22, 2016
Sponsors: Syracuse Univ., National Inst. of Aerospace, Utah Univ., ASTM International, National Agency for Finite Element Methods and Standards, American Society for Composites
Funding Number(s)
WBS: WBS 794072.02.07.03.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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