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Crack layer theory

The following simplified explanation for the observed power-law behaviour during stick-slip crack growth is a limiting case of a more general approach to SCG [43] based on crack layer theory [40, 41]. The crack layer in... [Pg.94]

In the crack layer theory (75,76) the movement of the crack and surrounding damage is decomposed into elementary movements translation, rotation, isotropic expansion, and distortion. In this way, the damage surrounding the tip can evolve in a general sense. These elementary movements become thermodynamic fluxes. The reciprocal forces contain an active part (energy release rates associated with each movement) Aj, and a resistive part (an energy barrier) Rt. Within the context of classical irreversible thermodynamics, the entropy of the system. Si, can be expressed in terms of a bilinear form of forces and fluxes shown in equation 27. [Pg.3071]

Chudnovsky, A., Crack Layer Theory, NASA Report, N174634 (1984)... [Pg.2444]

PZ constitute Crack Layer (CL) [6-8] and the rates of the crack and PZ growth characterize the kinetics of CL evolution. It is controlled by thermodynamic forces associated with crack and PZ respectively [8]. In this p er, a numerical algorithm and analysis of SCG computer simulations for PE is proposed based on CL theory. In addition, the lifetime of pipe is evaluated for various stress level, and the crack origin (inclusion) sizes and the locations. It leads to determination of the lower and upper boundary of the pipe grade PE lifetime in brittle fracture. [Pg.2441]

Figure 4. Flow chart of the computation program for the prediction of slow crack growth (SCG) based on the crack layer (CL) theory... [Pg.2445]

General hydrodynamic theory for liquid penetrant testing (PT) has been worked out in [1], Basic principles of the theory were described in details in [2,3], This theory enables, for example, to calculate the minimum crack s width that can be detected by prescribed product family (penetrant, excess penetrant remover and developer), when dry powder is used as the developer. One needs for that such characteristics as surface tension of penetrant a and some characteristics of developer s layer, thickness h, effective radius of pores and porosity TI. One more characteristic is the residual depth of defect s filling with penetrant before the application of a developer. The methods for experimental determination of these characteristics were worked out in [4]. [Pg.613]

Other theories proposed dissipation of energy through crack interaction localised heating causing the material to be raised to above the glass transition temperature in the layers of resin between the rubber droplets and a proposal that extension causes dilation so that the free volume is increased and the glass transition temperature drops to below the temperature of the polyblend. [Pg.56]

The usual form of the BET isotherm is derived for the case of a free (exposed) surface, where there is no limit on the number of adsorbed layers that may form. Such an assumption is clearly not good for a very porous adsorbent, such as one with deep cracks having a width of a few monolayer thicknesses, since the surface of these cracks can hold only a few layers even when the cracks are filled. Eortunately, the BET theory is most reliable at low relative pressures (0.05 to 0.3), at which only a few complete layers have formed, and it can be applied successfully to the calculation of even for porons solids. [Pg.309]

The experimental observation that there exists a critical thickness above which cracking occurs cannot easily be explained. Brinker [1] discusses a theory which explains that very thin layers can bear much larger stresses because critical cracks carmot be formed unless a certain critical thickness is surpassed. This thickness is estimated to be equal to or less than 1 pm and Brinker comes to the conclusion that thicker films will always crack. This is certainly not the case for alumina, titania and zirconia films for which much larger (alumina) to larger (titania) thicknesses are observed. As shown in Table 8.2 critical thicknesses of a few pm in single-step dip-coated films occur and critical flaws are smaller than this thickness and so can be present. [Pg.296]


See other pages where Crack layer theory is mentioned: [Pg.74]    [Pg.228]    [Pg.232]    [Pg.3070]    [Pg.440]    [Pg.74]    [Pg.228]    [Pg.232]    [Pg.3070]    [Pg.440]    [Pg.192]    [Pg.75]    [Pg.897]    [Pg.898]    [Pg.910]    [Pg.2441]    [Pg.210]    [Pg.374]    [Pg.260]    [Pg.1243]    [Pg.102]    [Pg.627]    [Pg.92]    [Pg.403]    [Pg.171]    [Pg.181]    [Pg.108]    [Pg.118]    [Pg.221]    [Pg.68]    [Pg.114]    [Pg.627]    [Pg.282]    [Pg.295]    [Pg.358]    [Pg.468]    [Pg.527]    [Pg.546]    [Pg.11]    [Pg.524]    [Pg.3]    [Pg.639]    [Pg.288]   
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