Effect of Curing Conditions on the Interface Strength of Single-Fibre Composite Specimens

2012 ◽  
Vol 54 (5) ◽  
pp. 335-339
Author(s):  
Murat Yavuz Solmaz ◽  
Mete Onur Kaman ◽  
Kadir Turan
1993 ◽  
Vol 2 (5) ◽  
pp. 096369359300200 ◽  
Author(s):  
H.D. Wagner ◽  
S. Ling

An energy balance approach is proposed for the single fibre composite (or fragmentation) test, by which the degree of fibre-matrix bonding is quantified by means of the interfacial energy, rather than the interfacial shear strength, as a function of the fibre geometrical and mechanical characteristics, the stress transfer length, and the debonding length. The validity of the approach is discussed using E-glass fibres embedded in epoxy, both in the dry state and in the presence of hot distilled water.


1993 ◽  
Vol 48 (1-4) ◽  
pp. 47-56 ◽  
Author(s):  
C. Baxevanakis ◽  
D. Jeulin ◽  
D. Valentin
Keyword(s):  

1996 ◽  
Vol 30 (14) ◽  
pp. 1514-1538 ◽  
Author(s):  
Devesh Tripathi ◽  
Fangping Chen ◽  
Frank R. Jones

1993 ◽  
Vol 2 (5) ◽  
pp. 096369359300200 ◽  
Author(s):  
H. D. Wagner ◽  
J. R. Wood ◽  
G. Marom

A novel technique was recently introduced in our laboratories for the measurement of the compressive strength of single fibres, based on a modified configuration of the single fibre composite fragmentation test. In particular, the effect of the length of the embedded fibre on its compressive strength was assessed for the first time, based on Weibull statistics considerations. Moreover, during the sample manufacturing stage, a fibre can break in compression due to induced cooling stresses, rather than mechanical stresses, which can be determined from the fragmentation phenomenon. In this note, improved analyses of such compressive fragmentation effects are presented and discussed.


1984 ◽  
Vol 19 (1) ◽  
pp. 43-49 ◽  
Author(s):  
J Ostrowski ◽  
G T Will ◽  
M R Piggott

Two methods have been used to evaluate the transverse stresses when an aligned fibre composite is stressed in the fibre direction. A single fibre model is shown to overestimate the stresses at the fibre-matrix interface by about 20 per cent compared with a finite element solution for an infinite array of fibres. Using relatively few fibres in the finite element analysis, however, only gives very approximate stress distributions. With fibre volume fractions in the range 0-0.50 the average radial stresses across the fibre-matrix interface are always compressive, and can be represented by a relatively simple formula with an accuracy which is normally with in a few percent of the finite element value.


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