2001
DOI: 10.1016/s0022-3093(01)00463-x
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Effect of oxidation treatment on the crack propagation rate of aerogels

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Cited by 13 publications
(10 citation statements)
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“…At low K I , V is two orders of magnitude higher for the hydrophilic gel. We note that n is identical in this K I range for the two samples, which means that the mechanism associated to crack propagation is the same; n is close to 15 and corresponds to a corrosion mechanism by OH À (Despetis et al 2001). At higher K I , n changes and becomes equal to 35, the classical n value found for vitreous silica, associated to a corrosion mechanism by water molecules (Suratwala and Steele 2003).…”
Section: Stress Corrosionmentioning
confidence: 53%
“…At low K I , V is two orders of magnitude higher for the hydrophilic gel. We note that n is identical in this K I range for the two samples, which means that the mechanism associated to crack propagation is the same; n is close to 15 and corresponds to a corrosion mechanism by OH À (Despetis et al 2001). At higher K I , n changes and becomes equal to 35, the classical n value found for vitreous silica, associated to a corrosion mechanism by water molecules (Suratwala and Steele 2003).…”
Section: Stress Corrosionmentioning
confidence: 53%
“…If the medium is basic, corrosive species are hydroxide ions and the activation energy of the reaction is changed: n value becomes equal to 15 [2]. However, for silica aerogels in contact with water vapor we observed two slopes in the region I [3,4]. Because these two domains are associated to two different corrosion mechanisms, we proposed that at low crack propagation rates (n = 15), hydroxide ions resulting from the dissociation of highly organized water molecules adsorbed on the gel surface, react with the silica network.…”
Section: Introductionmentioning
confidence: 79%
“…The experimental details have been reported in previous papers [3,4]. The crack growth rates have been measured within the range 10 À6 -10 À3 m/s with optical devices allowing us to estimate a change in the crack tip length of about 10 lm.…”
Section: Experimental Set-up For the Stress Corrosion Testmentioning
confidence: 99%
“…The literature explains that some monolithic aerogels can cracks several months later because of subcritical flaw propagation (Etienne et al 1995;Despetis et al 2001). This behavior being the results of internal stresses and progressive rupture of siloxane bonds by the action of water at the tip of the flaws.…”
Section: Textural Properties Of Nanocomposites Aerogelsmentioning
confidence: 99%