Statistical changes during the corrosion of glass fibre bundles

1988 ◽  
Vol 23 (8) ◽  
pp. 2926-2930 ◽  
Author(s):  
K. E. Evans ◽  
B. D. Caddock ◽  
K. L. Ainsworth
Keyword(s):  
Glass Fibre ◽  
Fibre Bundles

Testing E-glass fibre bundles using acoustic emission

1991 ◽  
Vol 26 (5) ◽  
pp. 1301-1310 ◽  
Author(s):  
A. Cowking ◽  
A. Attou ◽  
A. M. Siddiqui ◽  
M. A. S. Sweet ◽  
R. Hill
Keyword(s):  
Acoustic Emission ◽  
Glass Fibre ◽  
Fibre Bundles

Predicting sizing dependent bending rigidity of glass fibre bundles in sheet moulding compounds

2006 ◽  
Vol 37 (10) ◽  
pp. 1773-1786 ◽  
Author(s):  
Dima Merhi ◽  
Véronique Michaud ◽  
Emmanuelle Comte ◽  
Jan-Anders E. Månson
Keyword(s):  
Glass Fibre ◽  
Bending Rigidity ◽  
Fibre Bundles

Investigation into the behaviour of hollow glass fibre bundles under compressive loading

2003 ◽  
Vol 34 (11) ◽  
pp. 1045-1052 ◽  
Author(s):  
Martyn Hucker ◽  
Ian Bond ◽  
Stephen Bleay ◽  
Sajad Haq
Keyword(s):  
Glass Fibre ◽  
Compressive Loading ◽  
Fibre Bundles ◽  
Hollow Glass

scholarly journals Vertically-aligned short E-glass fibre core sandwich composite: Production and evaluation

2021 ◽  
pp. 109963622199388
Author(s):  
Robbie White ◽  
Venkata R Machavaram ◽  
Benjamin A Fernando ◽  
Mark A Paget ◽  
Ashwini Prasad ◽  
...  
Keyword(s):  
Compressive Strength ◽  
Glass Fibre ◽  
Failure Modes ◽  
Fibre Composite ◽  
Sandwich Panels ◽  
Sandwich Composite ◽  
Fibre Bundles ◽  
The Core ◽  
Vertically Aligned ◽  
Honeycomb Cores

This paper reports on the production and evaluation of a new class of “Z-axis” composite sandwich panel where the core consists of a dense array of vertically-aligned, 3 mm long E-glass fibre composite “beams”. The E-glass fibre bundles were aligned using electrostatic charging. A procedure was developed to retain the orientation of the short-fibre bundles whilst they were impregnated and cured with an epoxy/amine resin system. The skins were manufactured from 4-ply carbon/epoxy prepregs with a layup sequence of (0,90)s. The out-of-plane compressive strength of these Z-axis composites was found to be 25.2 and 15.2 times greater than equivalent sandwich panels made with Nomex® and aluminium honeycomb cores respectively. Their compressive strength was found to increase in proportion to the density of the core. Buckling and fracture of the vertically-aligned Z-axis composite were the predominant failure modes observed. The shear and flexural properties of the Z-axis composites were comparable to equivalent honeycomb sandwich panels manufactured from Nomex® and aluminium honeycomb cores.

Fracture resistance of root filled molar teeth restored with glass fibre bundles

2010 ◽  
Vol 43 (5) ◽  
pp. 356-362 ◽  
Author(s):  
F. B. Rodrigues ◽  
M. P. G. Paranhos ◽  
A. M. Spohr ◽  
H. M. S. Oshima ◽  
B. Carlini ◽  
...  
Keyword(s):  
Glass Fibre ◽  
Fracture Resistance ◽  
Fibre Bundles ◽  
Molar Teeth

Stress-corrosion failure envelopes for E-glass fibre bundles

1990 ◽  
Vol 25 (5) ◽  
pp. 2498-2502 ◽  
Author(s):  
B. D. Caddock ◽  
K. E. Evans ◽  
D. Hull
Keyword(s):  
Stress Corrosion ◽  
Glass Fibre ◽  
Corrosion Failure ◽  
Fibre Bundles ◽  
Failure Envelopes

Internal structure and fatigue performance of quasi-unidirectional non-crimp fabric reinforced laminates

2017 ◽  
Vol 51 (24) ◽  
pp. 3405-3423 ◽  
Author(s):  
Samuli Korkiakoski ◽  
Essi Sarlin ◽  
Reija Suihkonen ◽  
Olli Saarela
Keyword(s):  
Fatigue Life ◽  
Internal Structure ◽  
Glass Fibre ◽  
Fatigue Performance ◽  
Slope Parameter ◽  
Test Results ◽  
Cross Sectional ◽  
Microscopy Imaging ◽  
Fibre Bundles ◽  
Out Of Plane

The aim of this work was to study the effect of stitch pattern and stitch tension on tension-tension fatigue performance of quasi-unidirectional non-crimp fabric reinforced glass-fibre/epoxy laminates. Internal structure variations of the laminates were characterised using cross-sectional microscopy imaging for the evaluation of fatigue test results. Reinforcements for the study were manufactured with three different stitch patterns and two different stitch tensions. Based on the results, the stitch pattern contributes to in-plane and out-of-plane waviness of fibres, as well as on the size and shape of the axial fibre bundles. The fatigue life and slope parameter of the fitted S-N curve were significantly dependent on the stitch pattern, while they were not dependent on the applied stitch tension.

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