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Loadings experiment

A.S. Appleton and J.S. Waddington, The Importance of Shock-Wave Profile in Explosive Loading Experiments, Acta Metall. 12, 956-957 (1964). [Pg.258]

The lower bound 0 in the integration refers to the time at which the first contact is made after attaining the fully relaxed state. The upper bound / is the actual time spent in the loading experiment when the load P(i) is recorded. [Pg.124]

The premise of the above analysis is the fact that it has treated the interfacial and bulk viscoelasticity equally (linearly viscoelastic experiencing similar time scales of relaxation). Falsafi et al. make an assumption that the adhesion energy G is constant in the course of loading experiments and its value corresponds to the thermodynamic work of adhesion W. By incorporating the time-dependent part of K t) into the left-hand side (LHS) of Eq. 61 and convoluting it with the evolution of the cube of the contact radius in the entire course of the contact, one can generate a set of [LHS(t), P(0J data. By applying the same procedure described for the elastic case, now the set of [LHS(t), / (Ol points can be fitted to the Eq. 61 for the best values of A"(I) and W. [Pg.127]

The ratio of third- to second-order piezoelectric constants has also been determined for x-cut quartz with the acceleration pulse loading method [77G05]. Two experiments yielded values for Cm/Cu of 15.0 and 16.6 compared to the ratio of 15.3 [72G03] determined from the fit to the 25 shock loading experiments. [Pg.81]

Once values for R , Rp, and AEg are calculated at a given strain, the np product is extracted and individual values for n and p are determined from Eq. (4.19). The conductivity can then be calculated from eq. (4.18) after the mobilities are calculated. The hole mobility is the principal uncertainty since it has only been measured at small strains. In order to fit data obtained from elastic shock-loading experiments, a hole-mobility cutoff ratio is used as a parameter along with an unknown shear deformation potential. A best fit is then determined from the data for the cutoff ratio and the deformation potential. [Pg.91]

The most distinctive aspect of the shock work is the determination of higher-order piezoelectric constants. The values determined for the constants are, by far, the most accurate available for quartz and lithium niobate, again due to the direct nature of the measurements. Unfortunately it has not been possible to determine the full set of constants. Given the expense and destructive nature of the shock experiment, it is unlikely that a full set of higher-order piezoelectric constants can be determined. A less expensive investigation of higher-order constants could be conducted with the ramp wave or acceleration wave loading experiment described in the chapter. [Pg.95]

In loading experiments the separation of the matrix from the filler is one of the reasons responsible for the deviation of the stretching diagram deviation from linearity are lower than in case of good adhesion [240]. For good adhesion, the value of e gradually decreases with increasing filler concentration if adhesion is poor, it remains invariant up to a certain concentration and then drops very suddenly. [Pg.37]

Significantly, a flexural specimen is not in a state of uniform stress. When a simply supported specimen is loaded, the side of the material opposite the loading undergoes the greatest tensile loading. The side of the material being loaded experiences compressive stress (Fig. 2-16). These stresses decrease linearly toward the center of the sample. Theoretically the center is a plane, called the neutral axis, experiences no stress. [Pg.56]

The Y-axis represents the magnitude of the friction signal force and the X-axis is the load. The slope of the trend line is dehned as the friction factor (friction force signal/load) which is used to express the relative friction coefficient (friction force/load). Experiments that have been done in the same monolayer L-B him but different scan ranges give similar results as shown in Fig. 24 and Fig. 25. The friction factors of this monolayer L-B him, 0.0265 and 0.0203, are similar. The topographies of these two areas are shown in Fig. 26. [Pg.199]

The total quantities of chlorine dioxide formed are quite low and are in the order of 0.5-3 g for the peak-load experiments. Because this is a relatively low range of values, it is not easy to discover any correlations with other species involved in the reactions as the concentration may hardly change. This could also be one of the reasons that there is no relationship found between chlorate and the C102 emission values. [Pg.325]

FIGURE 8.2 Tensile loading experiments performed on single fibers embedded in a matrix. The illustration on the left is preapplication of the tensile loading and those on the right are postapplication of the tensile loading. [Pg.241]

Pool-Loading Experiments and Possibility that Reduction in Incorporation Reduces Influx into Soluble Pool. In order to empirically eliminate the possibility that the observed reduction in uptake of labelled amino acids into the soluble pool was an indirect result of an inhibition of incorporation, it was necessary to experimentally separate the influx and incorporation systems in vivo. The operational compromise required to accomplish this has been given by Sacher (55), and involves in the present case measuring the rates of label incorporation in control and treated tissues which have had their soluble pools fully loaded with unlabelled amino acid. Thus, the label-specific... [Pg.141]

The same molecular mechanisms as in tensile drawing are observed, of course, in constant load experiments. Depending on the stress-time-temperature regime essentially four different failure modes are observed with thermoplastic materials ... [Pg.12]

In Figure 5 an over-loading experiment is depicted (Schurig et al., 1990). The second fraction was eluted by increasing the temperature to 70°C. Incidentally, this leads to peak splitting due to temperature fluctuations in the oven (thermal christmas-tree -effect). [Pg.272]

Figure 5. Over-loading experiment of 5 - 30 /il 2,2-dimethyl-3-phenyloxirane on Mn-CAM2 (experimental conditions cf, text). Figure 5. Over-loading experiment of 5 - 30 /il 2,2-dimethyl-3-phenyloxirane on Mn-CAM2 (experimental conditions cf, text).
Figure 15. Over-loading experiment (column B) with incremental additions of racemic PHTP (Schiirch et al., 2001). Figure 15. Over-loading experiment (column B) with incremental additions of racemic PHTP (Schiirch et al., 2001).
Figure 18. Left Temperature-programmed preparative-scale separation of racemic enflurane by GC. Injected amount 30 /A, 8.4 cm/s helium. Bight Over-loading experiment at 40°C and 8.4 cm/s helium (Schurig and GTosenick, 1994). Figure 18. Left Temperature-programmed preparative-scale separation of racemic enflurane by GC. Injected amount 30 /A, 8.4 cm/s helium. Bight Over-loading experiment at 40°C and 8.4 cm/s helium (Schurig and GTosenick, 1994).
The infrared spectrum (v(CO) 2046 and 1969 cm 1) was again consistent with the presence of the desired polymer-bound complex, [Ir(CO)2I2]. ICP mass spectroscopic analysis of the metal loaded resins showed the metal contents to be 0.56-0.66 % (Rh) and 0.79-0.86 % (Ir) by weight. These values are in line with the observation that virtually all the metal complex is taken up from solution under the conditions of these loading experiments, and that 15-20% of the pyridinium sites are loaded with metal in the products. [Pg.168]

Fig. 6.15 Flow chart outlining how the dynamic frictional shear stress, rd, in fiber-reinforced ceramics can be calculated from cyclic loading experiments. Fig. 6.15 Flow chart outlining how the dynamic frictional shear stress, rd, in fiber-reinforced ceramics can be calculated from cyclic loading experiments.
Liquid loading experiments verified functional dependences and gave v ue of M, membrane mass per unit area experimental value of is then S = /2M. Value of M is based on composite membrane thickness and densities. Sm is then given by Sm = ITM. [Pg.143]

Plots of strain versus time for a creep experiment were shown previously in Figure 13-75 and in this constant load experiment the strain obtained from each of the components can be simply summed to give Equation 13-92 ... [Pg.461]

GPa. Recently, a direct tensile-loading experiment using individual MWNT mounted between two opposing AFM tips that can be stress-loaded inside a scanning electron... [Pg.5978]

Figure 27 (a) Stress versus strain curves of different SWNTs ropes obtained in tensile-loading experiments carried out using AFM for eight ropes of SWNTs having diameter from 19 to 41 nm. (Reprinted with permission from M.-F. Yu, B.S. Files, S. Arepalli, and R.S. Ruoff, Phys. Rev. Lett., 2000, 84, 5552. 2000 by the American Physical Society.) (b) Stress versus strain curves for individual MWNTs. (Reprinted with permission from M.-F. Yu, O. Lourie, M.J. Dyer, K. Moloni, T.F. Kelly, and R.S. Ruoff, Science, 2000, 287, 637. 2000 AAAS)... [Pg.5979]

Fig. 5. Results for G c calculated from different thermomechanical loading experiments in comparison with the critical value of G c,mm = 0.17 N/mm and with an indication of the cooling rates... Fig. 5. Results for G c calculated from different thermomechanical loading experiments in comparison with the critical value of G c,mm = 0.17 N/mm and with an indication of the cooling rates...

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