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Ceramic critical crack size

Tensile Strength of Ceramic Components, and Critical Crack Size... [Pg.544]

Strength test results on ceramic specimens show, in general, a large scatter. This follows from the fact, that in each individual specimen, the size of the critical crack is a little different. Rearranging Eq. (8) provides a relationship for the critical crack size (Griffith crack size) in a specimen ... [Pg.544]

Shelty s Criteria. The critical crack size relative to the size of the stressconcentrating defect is the key parameter determining the effect of stress-state on flaw severity. The relative critical crack size is a parameter of the material. In commercial aluminas it is 2 to 3 times the pore size. In RBSN it is much smaller. (D.K. Shetty et al, in Fracture Mechanics of Ceramics 5, Bradt et al. Plenum 1983, p 531). See... [Pg.283]

SCF precracks are especially sensitive to stable crack extension from environmental effects. Reference 18 shows examples for alumina and several other ceramics. C 1421 recommends that the precracks be examined for fractographic evidence of stable extension and if it is detected, the critical crack size should be used for the fracture toughness calculation. Testing in inert atmospheres is effective in eliminating the interference in SCF testing. [Pg.315]

For many ceramic materials, the ratio JQ/oy is of the order 1/100 /Tn. If a fracture starts in the interior of the component, the geometric correction factor for a pennyshaped crack (7 = 2/jt) can be used to calculate the corresponding Griffith crack size, giving a typical 80 pm. The size of critical flaws reflects the state of the art in... [Pg.544]

Also referred to as median vent cracks, these are caused to pop-in by exceeding a critical indenter load. It is the pop-in phenomenon that is important to the development of this subject in ceramic science because the halfpenny crack has the surface trace which allows opaque materials to be analyzed by recording the radial crack size as a function of increasing load. There is, however, the implication that the surface must be prepared carefully by polishing to an optical finish in order to see the radial cracks. If necessary, samples must be annealed to remove polishing stresses. Radial cracks are the result of surface tensile stresses, (Xyy in equation (1.29). Such stresses are at a maximum at the elastic-plastic boundary. [Pg.85]

As stated in Section 5.2.1.4, when considering Palmqvist cracks, ceramics can produce shallow radials without prior formation of median cracks, and then a new stress distribution is used to anticipate this situation such that L in equation (5.80) becomes 1.577a the result is that equation (5.81) is rewritten as equation (5.83) while the critical flaw size is left as equation (5.82) describes... [Pg.270]

Kolhe, R., Wi, C.Y.I., Ustandag, E. and Sass, S.L., Residual thermal stresses and calculation of the critical metal particle size for interfacial crack extension in metal-ceramic matrix composites , Acta Mater, 1996 44(1) 279-287. [Pg.305]

Alternative approaches, termed indentation thermal shock tests , with pre-cracks of known sizes have been used by several authors to assess thermal shock damage in monolithic ceramics. Knoop (Hasselmann et al., 1978 Faber etal, 1981) or Vickers (Gong etal., 1992 Osterstock, 1993 Andersson and Rowcliffe, 1996 Tancret and Osterstock, 1997 Collin and Rowcliffe, 1999, 2000 Lee et al., 2002) indentations were made on rectangular bars, which were then heated to pre-determined temperatures and quenched into water. Crack extensions from the indentations were measured as a function of quench temperature differential, and the critical temperature for spontaneous crack growth (failure) was determined for the material. Fracture mechanics analyses, which took into account measured resistance-curve (7 -curve) functions, were then used to account for the data trends. [Pg.409]

In tension we are concerned with the largest crack, the critical flaw, particularly if it is on the surface. In compression we are concerned with the average flaw size, c. We can estimate the compressive stress to failure by substituting Cav into Eq. 16.5 and using a multiplier between 10 and 15. Teeth are ceramic composites they survive for years even when many cracks are present. [Pg.297]


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