Energy release rate prediction for delamination versus echelon crack advance under global mode III loadings

2017 ◽  
Vol 207 (2) ◽  
pp. 161-179
Author(s):  
Allison L. Horner ◽  
Barry D. Davidson
1981 ◽  
Vol 48 (1) ◽  
pp. 194-195
Author(s):  
C. Yatomi

We show that for a Mode III crack starting from the apex of a wedge, the initial value of the energy-release rate is zero, although the stresses at the crack tip are unbounded.


1995 ◽  
Vol 29 (16) ◽  
pp. 2108-2133 ◽  
Author(s):  
B. D. Davidson ◽  
R. Kruger ◽  
M. König

Results are presented from a theoretical investigation of the effects of stacking sequence on the energy release rate in laminated composite end-notched flexure test specimens. Deflections and energy release rates of unidirectional and multidirectional ENF specimens are obtained by classical laminated plate theory, shear deformable plate theory, and three dimensional finite element analyses. It is shown that the distribution of energy release rate varies across the front of an initially straight delamination. The percentage of mode II and mode III energy release rates for the specimen, as well as the local peak values of the mode II, mode III and total energy release rates that occur at the specimen's free edges are shown to correlate with a nondimensional ratio comprised of the specimen's flexural rigidities. The results of the study are used as a basis for a proposed “ENF test design procedure” that may be used for the determination of appropriate specimen stacking sequences and test geometries for studying delamination growth at interfaces between plies at various orientations. The test design procedure minimizes the contributions to the energy release rate from residual thermal stresses, geometric nonlinearities, local mode II concentrations at the specimen's free edges and local mode III effects.


2021 ◽  
pp. 002199832110201
Author(s):  
Pietro Sabbadin ◽  
Christian Berggreen ◽  
Brian Nyvang Legarth ◽  
Lujin Lin

This work presents a novel test fixture for mode III fracture characterization of delaminations in monolithic laminates and face-core debonds in foam core composite sandwich specimens. The test fixture is configured as an extension of the already existing shear-torsion-bending (STB) test designed for monolithic laminates. The specimen sizing, lay-up configuration and the manufacturing process are presented. Accordingly, an overview of the test fixture is provided along with the data reduction method employed to compute the energy release rate. The results from representable fracture characterization tests are presented as force vs. displacement curves, where different definitions of the critical load for crack propagation can be defined. Thus, the critical value of the energy release rate is computed using analytically based equations for the different definitions given for the critical loads. The results show a stable crack growth for monolithic laminate specimens. However, a highly non-linear response of the sandwich specimens, before the onset of crack propagation, is observed. A non-linear numerical analysis and destructive specimen inspections are carried out in order to identify the source of the non-linear behaviour observed in the experimental results.


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