Mode I Traction-Separation Relationship of Sylgard 184: Aluminum Interface Using Rigid Double Cantilever Beam Analysis

Author(s):  
Sreehari Rajan ◽  
Michael A. Sutton ◽  
William McMakin ◽  
Mike Steinzig ◽  
Laura Inkret ◽  
...  
2000 ◽  
Vol 123 (2) ◽  
pp. 191-197 ◽  
Author(s):  
Y. Shindo ◽  
K. Horiguchi ◽  
R. Wang ◽  
H. Kudo

An experimental and analytical investigation in cryogenic Mode I interlaminar fracture behavior and toughness of SL-E woven glass-epoxy laminates was conducted. Double cantilever beam (DCB) tests were performed at room temperature (R.T.), liquid nitrogen temperature (77 K), and liquid helium temperature (4 K) to evaluate the effect of temperature and geometrical variations on the interlaminar fracture toughness. The fracture surfaces were examined by scanning electron microscopy to verify the fracture mechanisms. A finite element model was used to perform the delamination crack analysis. Critical load levels and the geometric and material properties of the test specimens were input data for the analysis which evaluated the Mode I energy release rate at the onset of delamination crack propagation. The results of the finite element analysis are utilized to supplement the experimental data.


1996 ◽  
Vol 5 (1) ◽  
pp. 096369359600500
Author(s):  
Rongzhi Li ◽  
Lin Ye ◽  
Yiu-Wing Mai

The mode I interlaminar fracture of Kevlar thread stitched GFRP laminates has been studied using double-cantilever-beam (DCB) tests. It was found that stitching density and patterns influence interlaminar fracture performance of composites mainly through the different failure mechanisms of stitch threads during crack propagation.


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