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Strain fiber

Eurther heat treatment in excess of 2000°C is referred to as graphitization. Eiber stmcture further densifies as molecular packing and orientation increase. At temperatures of 3000°C or above, the fiber stmcture begins to approach a truly graphitic stmcture with three-dimensional order. Typically, fiber strain to failure decreases as the carbonization temperature exceeds 1500°C because of reaction of impurities with the carbon fiber and the development of an increasingly flaw-sensitive graphitic stmcture (31,34)... [Pg.5]

Data analysis routines may change with time, and it is desirable to be able to reanalyze old data with new analysis software. Our tensile test analysis software creates plots of engineering stress as a function of engineering strain, as illustrated in Figure 3. Our flexure test software plots maximum fiber stress as a function of maximum fiber strain, with the option of including Poisson s ratio in the calculations. Both routines generate printed reports which present the test results in tabular form, as illustrated in Figure 4. [Pg.50]

Fig. 2.9. Variation of the position of the 1580 cm peak with fiber strain (a) for a polyacrylonitrile (PAN)-bascd HMS4 carbon fiber, and (b) for Thornel 50 carbon fiber. After Robinson et al. (1987). Fig. 2.9. Variation of the position of the 1580 cm peak with fiber strain (a) for a polyacrylonitrile (PAN)-bascd HMS4 carbon fiber, and (b) for Thornel 50 carbon fiber. After Robinson et al. (1987).
Fig. 2,10. Fiber strain and interfacial shear stress (IFSS) profiles along the fiber length for a heat-treated Kevlar 49 fiber-epoxy resin composite. At applied strains of (a) 0.60% (b) 1.90% and (c) 2,5%. After... Fig. 2,10. Fiber strain and interfacial shear stress (IFSS) profiles along the fiber length for a heat-treated Kevlar 49 fiber-epoxy resin composite. At applied strains of (a) 0.60% (b) 1.90% and (c) 2,5%. After...
Prinzen FW, Augustijn CH, Arts T, Allessie MA, Reneman RS. Redistribution of myocardial fiber strain and blood flow by asynchronous activation. Am. J. Physiol. 1990 259 H300-8. [Pg.65]

Table 13.4 Average Fiber Strain-to-Failure as Measured by Full- and Subscale Ring Tests... Table 13.4 Average Fiber Strain-to-Failure as Measured by Full- and Subscale Ring Tests...
The basic assumption of this equation is that fiber strain, c/ is equal to the matrix strain, cm for any given stress applied to the composite. This assumption is reasonable for metal-metal systems but not for plastic or elastomer systems where the matrix has significantly lower modulus than the fiber. [Pg.534]

The exact laws, based on continuum analysis of the fibers and the matrix, would be very complicated. The analysis would involve equilibrium of stresses around, and in, the fibers and compatibility of matrix deformation with the fiber strains. Furthermore, end and edge effects near the free surfaces of the composite material would introduce complications. However, a simplified model can be developed for the interior of the composite material based on the notion that the fibers and the matrix interact only by having to experience the same longitudinal strain. Otherwise, the phases behave as two uniaxially stressed materials. McLean5 introduced such a model for materials with elastic fibers and he notes that McDanels et al.6 developed the model for the case where both the fibrous phase and the matrix phase are creeping. In both cases, the longitudinal parameters are the same, namely... [Pg.310]

Figure 16.14. Fiber strain vs. distance along composite recalculated from stress-induced Raman band shifts. [Adapted, by permission, from Young R J, Prog. Rubb. Plast. Technol., H, No.2,1995, 124-36.]... Figure 16.14. Fiber strain vs. distance along composite recalculated from stress-induced Raman band shifts. [Adapted, by permission, from Young R J, Prog. Rubb. Plast. Technol., H, No.2,1995, 124-36.]...
A study of five monoecious fiber strains grown in France showed two cannabinoid types one with 0.34% THC and... [Pg.180]

The blends were prepared in a twin-screw extruder. The spiral flow was determined at a melt temperature of 288°C (550°F) for the PC and 266°C (510°F) for the transparent DB. The mold release energy was determined by measuring the force required to eject a disc measuring 76 mm in diameter and 3.2 mm thick with 6.4 mm high ribs. The chemical resistance was determined by measuring the maximum allowable outer fiber strain on 2.0 mm tensile bars, which did not reduce tensile elongation. [Pg.851]

The heat distortion temperature (HDT) is the temperature Thd (in °C), at which a peripheral fiber strain of 0.2 % is reached. [Pg.74]

It can be concluded that both the temperature and strain stress enable the structural reorganization and orientation of the polymer, but the forced withdrawal shows stronger orientation effects than the SHMM under constant loadings. Only concrete tests of the fibers strain-strength properties can arbitrate which samples are more optimally orientated and with less micro destructions. [Pg.112]

This is the most widely used texturing process and accounts for about 90% of the textured filament yarn market. In this technique (Fig. 1.6b), twist is inserted into a heated multifilament yarn running at high speed. The yarn is cooled in the twisted state, so that the twist geometry is set, and then the yarn is untwisted. The insertion of twist distorts the fibers, strains the bonds within them, and causes them to break when heat is supplied. Cooling the yarn in the distorted state allows new bonds to form and stabilize the distorted configuration. In false-twist texturing, fiat, fully drawn multifilament yarn is twisted and passed over a heater maintained at a temperature well... [Pg.197]

Fig. 6.83 Transmission electron micrographs of samples subjected to creep deformation showing the formation of voids, a Tension side of a sample of 1.8-pm grain size with a totai of —3.5 % outer fiber strain. Cavities at tripie points can be seen. Arrows indicate stress axes, b A higher magnification micrograph of the sampie in (a) showing typicai eiongated cavities formed at triple points. Stress axes are indicated by arrows, c An electron micrograph of the same sample from the compression side. Note that there are very few cavities in comparison to the tension side, d A sample of 19-pm grain size showing numerous cavities (tension side, —3 % strain) note that... Fig. 6.83 Transmission electron micrographs of samples subjected to creep deformation showing the formation of voids, a Tension side of a sample of 1.8-pm grain size with a totai of —3.5 % outer fiber strain. Cavities at tripie points can be seen. Arrows indicate stress axes, b A higher magnification micrograph of the sampie in (a) showing typicai eiongated cavities formed at triple points. Stress axes are indicated by arrows, c An electron micrograph of the same sample from the compression side. Note that there are very few cavities in comparison to the tension side, d A sample of 19-pm grain size showing numerous cavities (tension side, —3 % strain) note that...
Shi, B., Zhang, D., Zhu, H.H., Liu, C. 2011. Application of distributed optical fiber strain measurement into geotechnical engineering monitoring. Proceedings of 8th International Workshop on Structural Health Monitoring, Stanford, 13-15 September. 2011. [Pg.627]

The failure of an r.c. column confined with composite materials occurs following failure of the composite fibers. Moreover, due to the disaggregation of confined concrete, the column loses its mechanical features and, thus, its strength against transversal forces. In order to prevent this state of degradation of concrete regulations, there is a call for a limit value of fiber strain of 0.004. [Pg.78]

One approach [3] is applicable to relatively dense assemblies of variously oriented fibers, in which the local fiber strain can be reasonably predicted from the global material strain by an affine deformation assumption. For nonwoven fabrics and twisted yarns, which are planar or quasi-planar (cylindrical) assemblies, the basic relations are ... [Pg.209]


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See also in sourсe #XX -- [ Pg.86 , Pg.87 , Pg.195 , Pg.199 ]




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